Aerospace and aviation technology Books
Springer-Verlag Berlin and Heidelberg GmbH & Co. KG Thermospheric Density and Wind Determination from
Book SynopsisThe Earth's atmosphere is often portrayed as a thin and finite blanket covering our planet, separate from the emptiness of outer space. In reality, the transition is gradual and a tiny fraction of the atmophere gases is still present at the altitude of low orbiting satellites. The very high velocities of these satellites ensure that their orbital motion can still be considerably affected by air density and wind. This influence can be measured using accelerometers and satellite tracking techniques. The opening chapters of this thesis provide an excellent introduction to the various disciplines that are involved in the interpretation of these observations: orbital mechanics, satellite aerodynamics and upper atmospheric physics. A subsequent chapter, at the heart of this work, covers advances in the algorithms used for processing satellite accelerometry and Two-Line Element (TLE) orbit data. The closing chapters provide an elaborate analysis of the resulting density and wind products, which are generating many opportunities for further research, to improve the modelling and understanding of the thermosphere system and its interactions with the lower atmosphere, the ionosphere-magnetosphere system and the Sun.Table of ContentsEmpirical modelling of the thermosphere.- Satellite dynamics and non-gravitational force modelling.- Producing density and crosswind from satellite dynamics observations.- Analysis and interpretation of density and wind data.- Empirical model calibration.- Conclusions and recommendations.
£85.49
Springer-Verlag Berlin and Heidelberg GmbH & Co. KG Onboard Computers, Onboard Software and Satellite
Book SynopsisThis book is intended as a system engineer's compendium, explaining the dependencies and technical interactions between the onboard computer hardware, the onboard software and the spacecraft operations from ground. After a brief introduction on the subsequent development in all three fields over the spacecraft engineering phases each of the main topis is treated in depth in a separate part.The features of today’s onboard computers are explained at hand of their historic evolution over the decades from the early days of spaceflight up to today. Latest system-on-chip processor architectures are treated as well as all onboard computer major components.After the onboard computer hardware the corresponding software is treated in a separate part. Both the software static architecture as well as the dynamic architecture are covered, and development technologies as well as software verification approaches are included.Following these two parts on the onboard architecture, the last part covers the concepts of spacecraft operations from ground. This includes the nominal operations concepts, the redundancy concept and the topic of failure detection, isolation and recovery.The baseline examples in the book are taken from the domain of satellites and deep space probes. The principles and many cited standards on spacecraft commanding, hardware and software however also apply to other space applications like launchers. The book is equally applicable for students as well for system engineers in space industry.Table of ContentsContext.- Onboard Computers.- Onboard Software.- Satellite Operations.
£170.99
Springer Fachmedien Wiesbaden Flugzeugtriebwerke: Grundlagen,
Book SynopsisDieses Buch bietet eine umfassende und detaillierte Behandlung der wichtigsten Fragen zu Flugzeug- und Gasturbinenantrieben für Ingenieure, ein hervorragendes Kompendium für fortgeschrittene Studenten. Es hat sich in kurzer Zeit einen herausragenden Platz in der Fachliteratur erobert.Eine leicht verständliche Einführung in die zugehörigen Aspekte der Aerodynamik und der Thermodynamik vereinfacht den Einstieg in die Theorie ganz erheblich und schafft so sichere Grundlagen. In weiteren Abschnitten werden entscheidende Begriffe und technisch/physikalische Zusammenhänge anschaulich definiert und parametrische Kreisprozessanalysen idealer und realer Triebwerke vorgestellt. Eine Klassifizierung der Flugzeugtriebwerke und Funktionsbeschreibungen der Hauptkomponenten fehlen ebenso wenig wie die Thermo- und Aerodynamik thermischer Turbomaschinen. Anhand zahlreicher durchgerechneter Beispiele wird der Einstieg in die verschiedenen Wege der Vorauslegung von Triebwerken uns dessen Komponenten eröffnet. Neu hinzugekommen ist ein Kapitel über Propeller- und Propellersysteme.Table of ContentsVorwort.- Formelzeichen.- Einführung.- Klassifizierung der Flugzeugtriebwerke.- Was man weiß - was man wissen sollte.- Hauptkomponentenbeschreibung und zugehörige Technologien.- Triebwerksschub.- Definitionen und Grundlagen.- Parametrische Kreisprozessanalyse idealer Flugzeugtriebwerke.- Thermische Turbomaschinen.- Triebwerkseinlauf.- Verdichter.- Brennkammer.- Turbine.- Schubdüse.- Reale Triebwerkskreisprozesse.- Triebwerkslärm.- Triebwerkssysteme.- Propeller und Propellersysteme.- Anhänge.- Sachwortregister.
£360.99
Springer-Verlag Berlin and Heidelberg GmbH & Co. KG Three-Dimensional Attached Viscous Flow: Basic
Book SynopsisViscous flow is treated usually in the frame of boundary-layer theory and as two-dimensional flow. Books on boundary layers give at most the describing equations for three-dimensional boundary layers, and solutions often only for some special cases.This book provides basic principles and theoretical foundations regarding three-dimensional attached viscous flow. Emphasis is put on general three-dimensional attached viscous flows and not on three-dimensional boundary layers. This wider scope is necessary in view of the theoretical and practical problems to be mastered in practice. The topics are weak, strong, and global interaction, the locality principle, properties of three-dimensional viscous flow, thermal surface effects, characteristic properties, wall compatibility conditions, connections between inviscid and viscous flow, flow topology, quasi-one- and two-dimensional flows, laminar-turbulent transition and turbulence. Though the primary flight speed range is that of civil air transport vehicles, flows past other flying vehicles up to hypersonic speeds are also considered. Emphasis is put on general three-dimensional attached viscous flows and not on three-dimensional boundary layers, as this wider scope is necessary in view of the theoretical and practical problems that have to be overcome in practice.The specific topics covered include weak, strong, and global interaction; the locality principle; properties of three-dimensional viscous flows; thermal surface effects; characteristic properties; wall compatibility conditions; connections between inviscid and viscous flows; flow topology; quasi-one- and two-dimensional flows; laminar-turbulent transition; and turbulence. Detailed discussions of examples illustrate these topics and the relevant phenomena encountered in three-dimensional viscous flows. The full governing equations, reference-temperature relations for qualitative considerations and estimations of flow properties, and coordinates for fuselages and wings are also provided. Sample problems with solutions allow readers to test their understanding.Trade Review“The book would be an appropriate resource for every student of aerodynamics. … The book is well structured, and the bibliography which partially follows the chapters and sections is comprehensive. In order to test the reader’s understanding of the material, each chapter is accompanied by various problems and their solutions. A lot of graphics, including colored pictures, illustrate the book very well.” (Jürgen Socolowsky, Mathematical Reviews, April, 2017)Table of ContentsIntroduction.- Properties of Three-Dimensional Attached Viscous Flow.- Equations of Motion.- Boundary-Layer Equations for Three-Dimensional Flow.- Boundary-Layer Integral Parameters.- Viscous Flow and Inviscid Flow Connections and Interactions.- Topology of Skin-Friction Fields.- Quasi-One-Dimensional and Quasi-Two-Dimensional Flows.- Laminar-Turbulent Transition and Turbulence.- Illustrating Examples.- Solutions of the Problems.
£85.49
Springer-Verlag Berlin and Heidelberg GmbH & Co. KG Flugzeugbaukunde: Eine Einführung in die
Book SynopsisDieser Buchtitel ist Teil des Digitalisierungsprojekts Springer Book Archives mit Publikationen, die seit den Anfängen des Verlags von 1842 erschienen sind. Der Verlag stellt mit diesem Archiv Quellen für die historische wie auch die disziplingeschichtliche Forschung zur Verfügung, die jeweils im historischen Kontext betrachtet werden müssen. Dieser Titel erschien in der Zeit vor 1945 und wird daher in seiner zeittypischen politisch-ideologischen Ausrichtung vom Verlag nicht beworben.Table of ContentsI. Der Luftverkehr.- 1. Geschwindigkeit und Häufigkeit.- 2. Zuverlässigkeit und Bequemlichkeit.- 3. Wirtschaftlichkeit.- II. Die Luftkräfte.- 4. Form- und Reibungswiderstand.- 5. Auftrieb.- 6. Induzierter Widerstand.- III. Das Flugwerk.- 7. Entwurf.- 8. Ausführung.- IV. Das Triebwerk.- 9. Schrauben.- 10. Motoren.- V. Das Flugzeug.- 11. Flugleistungen.- 12. Flugeigenschaften.
£52.24
Springer-Verlag Berlin and Heidelberg GmbH & Co. KG Fluglehre: Theorie und Berechnung der Flugzeuge in elementarer Darstellung
Book SynopsisEntwicklung des Flugwesens und der Fluglehre, Rekordtabelle.- I. Allgemeines über Luftkräfte. Luftwiderstand.- 1. Luftdruck.- 2. Luftdichte.- 3. Inkompressible Strömung.- 4. Kompressible Strömung.- 5. Luftwiderstand in Unterschallströmung.- 6. Luftwiderstand in Überschallströmung.- 7. Widerstandsbeizahlen verschiedener Körper.- II. Die Tragfläche.- 8. Luftkräfte auf die Tragfläche.- 9. Querschnitt der Tragflügel.- 10. Grundriß der Tragflügel.- 11. Die Tragfläche in Überschallströmung.- 12. Der Aufbau der Tragflächen.- 13. Der Gleitflug.- III. Motorloser Flug.- 14. Fliegen aus eigener Kraft.- 15. Segelfliegen.- 16. Segelflugzeuge.- IV. Die Luftschraube.- 17. Die Wirkungsweise der Luftschraube.- 18. Die Kennlinien von Verstellschrauben.- 19. Herstellung und Prüfung der Luftschrauben.- V. Das Triebwerk.- 20. Allgemeines über Flugzeugtriebwerke.- 21. Kolbentriebwerke und ihre Kennlinien.- 22. Aufbau der Kolbenmotoren und ihre Einzelteile.- 23. Strömungstriebwerke und ihre Kennlinien.- 24. Aufbau der Gasturbinentriebwerke und ihre Einzelteile.- VI. Flugleistungen.- 25. Waagrechtflug.- 26. Steigflug.- 27. Reichweite.- 28. Messung der Flugleistungen.- VII. Steuemng und Stabilität.- 29. Flossen, Ruder, Steuerungen.- 30. Wirkung der Ruder.- 31. Längs- und Querstabilität.- 32. Automatische Flugzeugsteuerung.- VIII. Abflug und Landung.- 33. Hilfsmittel für Abflug und Landung.- 34. Der Abflugvorgang.- 35. Der Landevorgang.- IX. Das Drehflügelflugzeug.- 36. Allgemeines über Schraubenflugzeuge.- 37. Der vertikale Flug.- 38. Der Vorwärtsflug.- 39. Blattbewegungen.- 40. Hubschraubersteuerung, Stabilität, Schwingungen.- X. Kursbestimmung und Flugbeförderung.- 41. Einfluß des Windes auf Kurs und Flugdauer.- 42. Funknavigation.- 43. Die direkten Kosten derFlugbeförderung.- 44. Einige neuere Flugzeugmuster.- Zusammenstellung der wichtigsten Bezeichnungen.- Namen- und Sachverzeichnis.- Zahlentafeln.- 1. Luftwiderstand verschiedener Querschnittsformen.- 2. Hauptabmessungen, Leistungen und Verbrauchszahlen einiger Flugmotoren.- 3. Hauptabmessungen, Leistungen und Verbrauchszahlen einiger Flugzeuggasturbinen.- 4. Abmessungen einiger neuzeitlicher Flugzeuge.- 5. Temperatur, Druck, Dichte, Schallgeschwindigkeit und Zähigkeit der Luft in der Normalatmosphäre.Table of ContentsEntwicklung des Flugwesens und der Fluglehre, Rekordtabelle.- I. Allgemeines über Luftkräfte. Luftwiderstand.- 1. Luftdruck.- Luftdruck in Meereshöhe.- Druckabnahme mit der Höhe.- Normalatmosphäre.- Barometrische Höhenmessung.- 2. Luftdichte.- Luftdichte in Meereshöhe.- Einfluß von Druck und Temperatur.- Zustandsgleichung für Gase.- Die wirkliche Atmosphäre.- Berichtigung der Steiggeschwindigkeit.- Umrechnung auf Normalatmosphare.- 3. Inkompressible Strömung.- Druck und Geschwindigkeit im Stromfaden.- Geschwindigkeitsmessung.- Staudruck.- Bernoullische Gleichung.- Impulssatz.- 4. Kompressible Strömung.- Machscher Kegel.- Schwache Verdichtungswelle.- Innere Wärmeenergie.- Energiesatz und adiabatische Zustandsänderung.- Schallgeschwindigkeit.- Wärmeinhalt (Enthalpie).- Energiesatz für Gasströmungen.- Verlustfreie Gasströmung.- Stautemperatur.- Staupunktsdruck und Staudruck.- Überschalldüse (Lavaldüse).- Gerader Verdichtungsstoß.- Stoßverluste.- Staudruck in Überschallströmung.- Überschallwelle.- 5. Luftwiderstand in Unterschallströmung.- Widerstand durch Wirbelbildung.- Reibungswiderstand.- Widerstandsbeiwer.- Reynoldssche Kennzahl.- Zähigkeitszahl.- 6. Luftwiderstand in Überschallströmung.- Wellenwiderstand.- Kleine Ablenkung der Überschallströmung.- Ablenkung um größere Winkel.- Wellenwiderstand des dünnen Doppelkeiles.- Wellenwiderstand der schwach angestellten Platte.- Widerstand in schallnahen Strömungen.- 7. Widerstandsbeizahlen verschiedener Körper.- Veränderlicbkeit der Widerstandsbeizahlen.- Widerstandsbeiwerte verschiedener Querschnittsformen.- Teilwiderstände am Flugzeug.- Oberflächenreibung.- Schlanke Körper und Flügelprofile.- Aerodynamischer Flugzeugwirkungsgrad.- II. Die Tragfläche.- 8. Luftkräfte auf die Tragfläche.- Aligemeines.- Anstellwinkel, Auftrieb und Rücktrieb.- Gleitzahl.- Druckverteilung über die Tiefe.- Abwärtsbeschleunigung der Luft.- Zirkulation.- Auftriebs- und Widerstandsbeiwert.- Tragflächenkennlinien.- 9. Querschnitt der Tragflügel.- Aufbau des Profils.- Höchstauftrieb und Kleinstwiderstand.- Kennlinien eines Profils.- Kennlinien für große Anstellwinkel. S.73.- Auftriebserhöhung durch Endklappen.- Auftriebserhöhung durch Schlitzvorflügel.- Endklappe mit Schlitz.- Weitere Mittel zur Auftriebserhöhung.- 10. Grundriß der Tragflügel.- Seitenverhältnis.- Flächenbelastung.- Wirbelkette.- Induzierte Abwärtsgeschwindigkeit.- Induzierter Widerstand.- 11. Die Tragfläche in Überschallströmung.- Die drei Verlustquellen.- Seitenverhältnis.- Näherungen für Auftrieb und Widerstand.- Gleitverhältnis.- Vergleich mit Unterschalltragflächen.- Pfeilstellung.- Überschallwindkanäle.- Überschallversuchsergebnisse.- Auftriebsschwingungen.- Langsamflugprobleme.- 12. Der Aufbau der Tragflächen.- Belastung der Tragfläche.- Tragflügelbauweisen und Baustoffe.- Sichere Last und Sicherheitsgrad.- Beschleunigungslasten (Abfangen).- Böenlasten.- Weitere Lastzustönde.- Belastungsversuch.- Ermüdungsfestigkeit.- Flattern von Tragflügeln.- 13. Der Gleitflug.- Schädlicher Widerstand und Auftriebsfaktor.- Dimensionslose Fluggeschwindigkeit.- Gleitzahlberechnung.- Gleitwinkel, Anstellwinkel, Fluglagenwinkel, Sinkgeschwindigkeit.- III. Motorloser Flug.- 14. Fliegen aus eigener Kraft.- Erforderliche und verfügbare Muskelleistung.- Zukunftsaussichten des Muskelfluges.- Vergleich mit dem Vogelflug.- 15. Segelfliegen.- Statisches Segeln.- Hangaufwind.- Thermischer Aufwind.- Aufwind in Leewellen.- Reibungsaufwind.- Dynamisches Segeln.- 16. Segelflugzeuge.- Segelflugrekorde. S. 115.- Verwendungsbereich.- Hauptabmessungen.- IV. Die Luftschraube.- 17. Die Wirkungsweise der Luftschraube.- Kräfte am Propellerelement.- Elementwirkungsgrad.- Blattsteigungswinkel.- Verstellbare Blätter.- 18. Die Kennlinien von Verstellschrauben.- Schub- und Drehmomentenbeiwert.- Aktivitätsfaktor.- Wirkungsgrad eines Luftstrahlantriebes.- Strahlwirkungsgrad des Propellers.- Windkanalmeßergebnisse.- Entwurf einer Luftschraube.- Vergleich der Verstellschraube mit der Festblattschraube.- 19. Herstellung und Prüfung der Luftschrauben.- Bauweisen der Blätter.- Blattverstellmechanismus.- Statische und dynamische Ausbalancierung.- Schwingungsbeanspruchungen.- Windkanalversuche.- V. Das Triebwerk.- 20. Allgemeines über Flugzeugtriebwerke.- Thermischer Wirkungsgrad.- Strömungstriebwerke und Kolbentriebwerke.- Idealisiertes Strömungstriebwerk.- Heizwert und Verbrennungstemperatur. S.141.- Strahlwirkungsgrad. S.145.- Idealisiertes Kolbentriebwerk.- Verbundtriebwerke.- Raketentriebwerke.- 21. Kolbentriebwerke und ihre Kennlinien.- Viertaktmotor.- Verdichtungsgrad und Mitteldruck.- Detonation und Oktanzahl.- Der Dieselmotor.- Motorenprüfstände.- Bodenleistung.- Dauerleistung und Kurzleistung.- Höhenleistung.- Brennstoffverbrauch.- 22. Aufbau der Kolbenmotoren und ihre Einzelteile.- Reihen- und Sternmotoren.- Hauptabmessungen, Leistungen und Verbrauchszahlen einiger Flugmotoren.- Bauarten mit Abgasturbine.- Einzelteile.- Zylinder und Kolben.- Ventile und Steuerung.- Zündanlage.- Kühlung.- Schmierung.- 23. Strömungstriebwerke und ihre Kennlinien.- Entwicklungstendenzen.- Die Luftstaudüse (Lorinantrieb).- Argus-Schmidt-Rohr.- Brennkammerverluste.- Veranderung der Betriebsbedingungen bei gleichen Machschen Zahlen.- Düsentriebwerk.- Kompressor- und Turbinenverluste.- Flugwindstau.- Querschnittsgröße.- Kennlinien für ein Düsentriebwerk.- Umrechnung für Höhe.- Kennlinien für ein Turbopropellertriebwerk. S.187.- 24. Aufbau der Gasturbinentriebwerke und ihre Einzelteile.- Einwellentriebwerke. S.188.- Zweiwellentriebwerke.- Kaltluftzusatz.- Hauptabmessungen, Leistungen und Verbrauchszahlen einiger Gasturbinen.- Einzelteile der Gasturbinen.- Kompressor.- Brennkammer.- Turbine. S.199.- Austrittsdüse. S.201.- VI. Flugleistungen.- 25. Waagrechtflug.- Widerstand und Düsenschub.- Widerstand und Propellerschub.- Überschallflug mit Düsenantrieb. S.207.- 26. Steigflug.- Steiggeschwindigkeit.- Anstellwinkel beim Steigen.- Höheneinfluß.- Steigzeit und Gipfelhöhe.- Tragflächengroßen- und Fluggewichtsänderungen. S.214.- 27. Reichweite.- Aufgabenstellung. S.216.- Propellerflugzeug. S.217.- Flughöhe und Reichweite.- Windeinfluß.- Brennstoffvorrat und Reichweite.- Düsenflugzeug.- Fluggeschwindigkeit und Reichweite.- 28. Messung der Flugleistungen.- Messung der relativen Fluggeschwindigkeit.- Messung der Steiggeschwindigkeit und Umrechnung auf Normalatmosphäre. S.227.- Fluggeschwindigkeit bei Wind.- Stoppdreieck. S.231.- VII. Steuemng und Stabilität.- 29. Flossen, Ruder, Steuerungen.- Übersicht der Achsenrichtungen. S.233.- Querruder.- Höhenruder.- Seitenruder.- Begriff der Stabilität. S.237.- Steuerbetätigungsorgane.- Steuerkräfte. S.241.- Größte Handkräfte.- Servosteuerungen.- Künstliche Steuerkrafterzeugung.- 30. Wirkung der Ruder.- Kräfte bei Ruderausschlag.- Bemessung des Höhenruders.- Trägheitsmoment.- Bemessung des Seitenruders.- Kurvenflug.- in die Kurve.- Kurven im Wind.- 31. Längs- und Querstabilität.- Momentengleichgewicht.- Schwerpunkt.- Längsmomentenbeiwert.- Maß für Längsstabilität.- Stabilität und Knüppelstellung.- Momente um Längsachse. S.261.- V-Stellung. S.262.- Stabilisierung im überzogenen Fluge.- 32. Automatische Flugzeugsteuerung.- Dynamische Stabilität.- Zwecke der automatischen Steuerung.- Hauptbestandteile der automatischen Steuerung.- Flugeigenschaftsmessungen.- VIII. Abflug und Landung.- 33. Hilfsmittel für Abflug und Landung.- Aligemeines. S.274.- Fahrgestell mit Sporn. S.275.- Fahrgestell mit Bugrad.- Zweiradfahrwerk.- Raddrücke.- Wasserflugzeug und Flugboot.- 34. Der Abflugvorgang.- Kräfte beim Anlauf.- Anlaufzeit und Anlaufweg.- Windeinfluß auf den Abflugvorgang.- Methoden zur Verringerung der Anlaufstrecke. S.284.- Abflug vom Wasser. S.287.- 35. Der Landevorgang.- Landetechnik.- Landestoß.- Wasserlandung.- Methoden zur Verringerung der Auslaufstrecke.- IX. Das Drehflügelflugzeug.- 36. Allgemeines über Schraubenflugzeuge.- Der Tragschrauber.- Der Hubschrauber mit mechanischem Schraubenantrieb.- Der Hubschrauber mit Reaktionsschraubenantrieb.- Kombinationshubschrauber.- Verwandlungshubschrauber. S.308.- Verwandlungshubschrauber. S.308.- 37. Der vertikale Flug.- Strahltheorie der Hubschraube.- Profilverluste.- Blattspitzenverluste.- Schwebeflugkennlinien.- Optimale Hubschraubenabmessungen. S.317.- Der vertikale Abstieg.- Einfluß der Bodennähe.- 38. Der Vorwärtsflug.- Induzierte Verluste im Vorwärlsflug.- Profilverluste im Vorwärtsflug.- Rotorkennlinien.- Vortriebswirkungsgrad des Rotors. S.329.- Einfluß von Starrflügel.- Einfluß von Propeller.- Hubschrauberflugleistungen.- 39. Blattbewegungen.- Kegelwinkel.- Blattschlagbewegung.- Blattschwenkbewegung.- Simultane Blattverstellung.- Zyklische Blattverstellung.- 40. Hubschraubersteuerung, Stabilität, Schwingungen.- Steuerung der Hubschrauber.- Stabilität der Hubschrauber.- Hubschrauberschwingungen.- Mechanische Instabilität.- Ermüdungsfestigkeit der Hubschrauber.- X. Kursbestimmung und Flugbeförderung.- 41. Einfluß des Windes auf Kurs und Flugdauer.- Gerade Flugbahn.- Geschlossene Flugbahn.- Rascheste Flugbahn bei gleichmäßigem Wind.- Rascheste Flugbahn bei ungleichmäßigem Wind.- 42. Funknavigation.- Übersicht der Navigationsmethoden.- Funkpeilung.- Das Decca-System.- Das Loran-System.- Radar als Navigationshilfe. S.367.- 43. Die direkten Kosten der Flugbeförderung.- Wirtschaftlichkeit des Flugtransportes.- Zuladung.- Nutzlast.- Beförderungskosten je Tonnenkilometer.- Zahlenbeispiele (Propellerflugzeug, Hubschrauber, Düsenflugzeug). S.377.- Andere Wirtschaftszwecke des Flugzeuges.- 44. Einige neuere Flugzeugmuster.- Flugzeugbauarten.- Reise. S.383.- Verkehr.- Militärischer Transport.- Langstreckenbomber. S.390.- Hubschrauber. S.391.- Bemerkungen zu Zahlentafel 4.- Zusammenstellung der wichtigsten Bezeichnungen.- Namen- und Sachverzeichnis.- Zahlentafeln.- 1. Luftwiderstand verschiedener Querschnittsformen.- 2. Hauptabmessungen, Leistungen und Verbrauchszahlen einiger Flugmotoren.- 3. Hauptabmessungen, Leistungen und Verbrauchszahlen einiger Flugzeuggasturbinen.- 4. Abmessungen einiger neuzeitlicher Flugzeuge.- 5. Temperatur, Druck, Dichte, Schallgeschwindigkeit und Zähigkeit der Luft in der Normalatmosphäre.
£52.24
Springer Fachmedien Wiesbaden Die neue ISO 9001:2015 in Kürze: Änderungen für
Book SynopsisMartin Hinsch vermittelt dem Leser das Wichtigste in Kürze zur Normenumstellung der neuen ISO 9001:2015. Zu jedem einzelnen Normenkapitel werden dazu alle wesentlichen Änderungen erklärt. Der Autor richtet sich damit vor allem an jene QM-Interessierten, die bereits Kontakt mit der alten ISO 9001:2008 hatten und nun knapp und präzise über alle für den betrieblichen Alltag wichtigen Neuerungen informiert werden möchten. Für detailliertere Informationen werden die Leser auf das Grundlagenwerk „Die neue ISO 9001:2015 – Ein Praxis-Ratgeber für die Normenumstellung“ von Martin Hinsch verwiesen.Table of ContentsWas Sie in diesem Essential finden können.- Einleitung.- Aufbau und Grundprinzipien der ISO 9001:2015.- Kapitelübergänge / Querverweisliste.- Kontext der Organisation.- Führung.- Planung.- Unterstützung.- Betrieb.- Bewertung der Leistung.- Verbesserung.- Was Sie aus diesem Essential mitnehmen können.
£9.99
Springer Fachmedien Wiesbaden Relativistische Effekte bei der
Book SynopsisTobias Schüttler stellt in diesem essential beide im Detail sehr anspruchsvollen Gebiete – Einsteins berühmte Relativitätstheorie und die Satellitenortung mit GPS und Galileo – in allgemein verständlicher Weise dar und erklärt die Einflüsse der Relativitätstheorie bei der Satellitennavigation ohne höhere Mathematik. Es werden auch die zu dieser Betrachtung wichtigen Formeln genannt und motiviert. Um die Einflüsse der Relativitätstheorie auf ein Satellitennavigationssystem wie das europäische Galileo zu verstehen, muss man sich mit dem konkreten Messvorgang bei der Ortung auseinandersetzen. Die Grundidee des Verfahrens ist einfach – die technische Umsetzung indes höchst komplex.Table of ContentsWie funktioniert Satellitennavigation?.- Was hat Einstein mit Satellitennavigation zu tun?.- Alles etwas genauer betrachtet.- Relativistische Korrekturen bei GPS und Galileo.- Ausblick: Die Galileo-Satelliten Doresa und Milena.
£9.99
Springer Fachmedien Wiesbaden Variable Pitot-Triebwerkseinlässe für
Book SynopsisIn diesem Open-Access-Buch wird gezeigt, wie kommerzielle Überschallflugzeuge die Nachfrage nach einem schnellen, flexiblen und sicheren Transportmittel erfüllen könnten, wenn sie im Vergleich zu früheren Anwendungen eine höhere Nachhaltigkeit durch einen verringerten Kraftstoffverbrauch bieten würden. Dazu könnte eine Luftwiderstandsreduktion ihrer Triebwerke durch die Verwendung variabler Pitot-Einlässe beitragen. Diese finden in der gegenwärtigen reinen Unterschallluftfahrt keine Anwendung, da deren erhöhte Masse sowie die eingeschränkte Zuverlässigkeit und Sicherheit das vorhandene aerodynamische Einsparpotenzial überwiegen. Daher untersucht Stefan Kazula, ob variable Pitot-Einlässe für den Überschallbetrieb bis Mach 1,6 konstruktiv umsetzbar sind, die luftfahrtspezifischen Standards für Sicherheit und Zuverlässigkeit erfüllen können und dabei eine Verbesserung der Nachhaltigkeit ermöglichen. Hierfür wird der Stand der Technik zu variablen Pitot-Einlässen sowie zur Konstruktionsmethodik dargestellt. Zudem wird der zugrundeliegende Konstruktionsansatz zur Erarbeitung eines sicheren und zuverlässigen Konzepts sowie seine Umsetzung vorgestellt. Table of ContentsEinleitung.- Einlässe strahlgetriebener Flugzeuge.- Methodik der Konzeptstudie.- Durchführung der Konzeptstudie.- Zusammenfassung und Ausblick.
£40.49
Springer Fachmedien Wiesbaden Systemleichtbau für die Luftfahrt
Book Synopsisessentials liefern aktuelles Wissen in konzentrierter Form. Die Essenz dessen, worauf es als „State-of-the-Art“ in der gegenwärtigen Fachdiskussion oder in der Praxis ankommt. essentials informieren schnell, unkompliziert und verständlich als Einführung in ein aktuelles Thema aus Ihrem Fachgebiet als Einstieg in ein für Sie noch unbekanntes Themenfeld als Einblick, um zum Thema mitreden zu können Die Bücher in elektronischer und gedruckter Form bringen das Fachwissen von Springerautor*innen kompakt zur Darstellung. Sie sind besonders für die Nutzung als eBook auf Tablet-PCs, eBook-Readern und Smartphones geeignet. essentials sind Wissensbausteine aus den Wirtschafts-, Sozial- und Geisteswissenschaften, aus Technik und Naturwissenschaften sowie aus Medizin, Psychologie und Gesundheitsberufen. Von renommierten Autor*innen aller Springer-Verlagsmarken.Dies ist ein Open-Access-Buch.Table of ContentsMotivation.- Klassischer Leichtbau.- Systemleichtbau mit Integration passiver Funktionen.- Systemleichtbau mit Integration aktiver Funktionen.
£9.99
Springer-Verlag Berlin and Heidelberg GmbH & Co. KG Controlling in der Luftfahrt: Ausgewählte
Book SynopsisLuftfahrtunternehmen befinden sich in einem Markt mit hohen Wachstumsraten, doch immer wieder erschüttern Krisen die Luftfahrt. Doch nicht nur krisenbedingte Nachfrageeinbrüche stellen Luftfahrtunternehmen vor Schwierigkeiten, auch die fortwährende Globalisierung und der zunehmende Marktwettbewerb - vor allem durch Low Cost Airlines - führen selbst in Wachstumszeiten immer wieder zu Insolvenzen von Luftfahrtunternehmen. Letztlich müssen sie im hart umkämpften Markt Strategien finden, um dauerhaft bestehen zu können. Als Lösungsansatz bildet das Controlling gerade auch für mittelständische Luftfahrtunternehmen eine notwendige Methodik, um die Effizienz der Unternehmung zu sichern.Dieses Buch zeigt Ihnen typische Controllinginstrumente, die sich gerade für den Mittelstand eignen. Neben der Deckungsbeitragsrechnung sind die Anwendung des Revenue Managements und der Einsatz von Kennzahlen diskutiert.
£9.99
Springer-Verlag Berlin and Heidelberg GmbH & Co. KG Industrial Aviation Management: A Primer in
Book SynopsisThis book outlines the structure and activities of companies in the European aviation industry. The focus is on the design, production and maintenance of components, assemblies, engines and the aircraft itself. In contrast to other industries, the technical aviation industry is subject to many specifics, since its activities are highly regulated by the European Aviation Safety Agency (EASA), the National Aviation Authorities and by the aviation industry standard EN 9100. These regulations can influence the companies’ organization, personnel qualification, quality management systems, as well as the provision of products and services. This book gives the reader a deeper, up-to-date insight into today's quality and safety requirements for the modern aviation industry. Aviation-specific interfaces and procedures are looked at from both the aviation legislation standpoint as well as from a practical operational perspective.Table of ContentsIntroduction.- Authorities and Organizations.- Regulations and Certifications.- Design and Development.- Maintenance Management.- Production Management and Support.- Production.- Maintenance.- Supply Chain Management.- Human Resource and Qualification.- Quality and Safety Management.
£104.49
Logos Verlag Berlin GmbH Identification and Augmentation of a Civil Light
Book Synopsis
£49.93
Sudwestdeutscher Verlag Fur Hochschulschriften AG Transonic Compressor Stages with Non-Axisymmetric
Book Synopsis
£55.12
AS Verlag Swiss Air: A day by day documentation
Book SynopsisThis account of Swissair's day-by-day history will serve as the basis of any future exploration of Switzerland's former national carrier, from its founding right up to the grounding of the fleet and ultimate demise of the company. Documented here is every significant corporate decision, along with previously little-known background information, a comprehensive overview of operational incidents, the airline's route network over seven decades, the countries Swissair served and types of aircraft it operated. In short, this book covers everything that made the legendary airline distinctive, in unprecedented scope. This new standard reference work records in precise detail and in easily comprehensible English both the history of civil aviation in Switzerland and the qualities that Swissair deemed important over its 70 years in existence. Rather than judge or assign blame, this book sticks strictly to the facts and figures that reflect the dedication of Swissair employees - from those in the cockpit and the cabin to those in marketing and technical services, both at home and abroad - to "their" airline, from the very early days right up until the final flight by a Swissair aircraft. In the process, the book injects new life into one of the most exciting chapters in the history of Swiss commerce.
£79.99
Wydawnictwo STRATUS, Artur Juszczak From the Voisin to the Mirage: 100 Years of
Book SynopsisFrom the very beginning of aviation in South America, French aircraft and aviators played a major part in the development of military flying in Peru. This exciting new book covers the use of French aircraft and the involvement of French designers, instructors and military thinking in the development of the Peruvian air force. From 'stick and string' biplanes through to supersonic jets, many of the most significant French types saw service in Peru and were involved in local conflicts, as detailed in this book. Profusely illustrated with many rare photographs and colour profiles of selected aircraft in Peruvian markings.
£19.00
Editorial Juventud, S.A. Nuestra vela latina
Book Synopsis
£22.06
Ediciones Paraninfo, S.A Helicopteros Manual Basico
Book Synopsis
£26.74
IBN After Germanwings: The Life of an Airline Pilot
Book Synopsis
£14.36
Springer Structural Analysis: With Applications to
Book SynopsisThe authors and their colleagues developed this text over many years, teaching undergraduate and graduate courses in structural analysis courses at the Daniel Guggenheim School of Aerospace Engineering of the Georgia Institute of Technology. The emphasis is on clarity and unity in the presentation of basic structural analysis concepts and methods. The equations of linear elasticity and basic constitutive behaviour of isotropic and composite materials are reviewed. The text focuses on the analysis of practical structural components including bars, beams and plates. Particular attention is devoted to the analysis of thin-walled beams under bending shearing and torsion. Advanced topics such as warping, non-uniform torsion, shear deformations, thermal effect and plastic deformations are addressed. A unified treatment of work and energy principles is provided that naturally leads to an examination of approximate analysis methods including an introduction to matrix and finite element methods. This teaching tool based on practical situations and thorough methodology should prove valuable to both lecturers and students of structural analysis in engineering worldwide. This is a textbook for teaching structural analysis of aerospace structures. It can be used for 3rd and 4th year students in aerospace engineering, as well as for 1st and 2nd year graduate students in aerospace and mechanical engineering.Trade ReviewFrom the reviews:“This textbook is based on courses given by both authors at Georgia, Tech and is aimed directly at the early years undergraduates. It succeeds admirably in meeting the students’ needs by including a plethora of set problems and worked examples. … Moreover the way is then open in later years to general weighted residual formulations and applications to nonlinear and non-self-adjoint problems which are powerful tools in modern numerical codes.” (G. A. O. Davies, Aeronautical Journal, March, 2011)Table of ContentsPart I Basic tools and concepts; 1 Basic Equations of Linear Elasticity .1.1 The concept of stress; 1.1.1 The state of stress at a point; 1.1.2 Volume equilibrium equations; 1.1.3 Surface equilibrium equations; 1.2 Analysis of the state of stress at a point; 1.2.1 Stress components acting on an arbitrary face; 1.2.2 Principal stresses; 1.2.3 Rotation of stresses; 1.2.4 Problems; 1.3 The state of plane stress; 1.3.1 Equilibrium equations; 1.3.2 Stresses acting on an arbitrary face within the sheet; 1.3.3 Principal stresses;1.3.4 Rotation of stresses; 1.3.5 Special states of stress; 1.3.6 Mohr's circle for plane stress; 1.3.7 Lamé's ellipse; 1.3.8 Problems; 1.4 The concept of strain; 1.4.1 The state of strain at a point; 1.4.2 The volumetric strain; 1.5 Analysis of the state of strain at a point; 1.5.1 Rotation of strains 1.5.2 Principal strains; 1.6 The state of plane strain; 1.6.1 Strain-displacement relations for plane strain; 1.6.2 Rotation of strains; 1.6.3 Principal strains; 1.6.4 Mohr's circle for plane strain; 1.7 Measurement of strains; 1.7.1 Problems; 1.8 Strain compatibility equations; 2 Constitutive Behavior of Materials; 2.1 Constitutive laws for isotropic materials; 2.1.1 Homogeneous, isotropic, linear elastic materials; 2.1.2 Thermal effects; 2.1.3 Problems; 2.1.4 Ductile materials; 2.1.5 Brittle materials; 2.2 Allowable stress; 2.3 Yielding under combined loading; 2.3.1 Tresca's criterion; 2.3.2 Von Mises' criterion; 2.3.3 Comparing Tresca's and von Mises' criteria;2.3.4 Problems; 2.4 Material selection for structural performance; 2.4.1 Strength design; 2.4.2 Stiffness design 2.4.3 Buckling design; 2.5 Composite materials; 2.5.1 Basic characteristics;2.5.2 Stress diffusion in a composite; 2.6 Constitutive laws for anisotropic materials; 2.6.1 Constitutive laws for a lamina in the fiber aligned triad; 2.6.2 Constitutive laws for a lamina in an arbitrary triad; 2.7 Strength of a transversely isotropic lamina; 2.7.1 Strength of a lamina under simple loading conditions; 2.7.2 The Tsai-Wu failure criterion; 2.7.3 The reserve factor; 3 Linear Elasticity Solutions; 3.1 Solution procedures; 3.1.1 Displacement formulation; 3.1.2 Stress formulation; 3.1.3 Solutions to elasticity problems; 3.2 Plane strain problems; 3.3 Plane stress problems; 3.4 Plane strain and plane stress in polar coordinates; 3.5 Problem featuring cylindrical symmetry; 3.5.1 Problems; 4 Engineering Structural Analysis; 4.1 Solution approaches; 4.2 Bar under constant axial force; 4.3 Hyperstatic systems; 4.3.1 Solution procedures; 4.3.2 The displacement or stiffness method; 4.3.3 The force or flexibility method; 4.3.4 Problems; 4.3.5 Thermal effects in hyperstatic system; 4.3.6 Manufacturing imperfection effects in hyperstatic system; 4.3.7 Problems; 4.4 Pressure vessels; 4.4.1 Rings under internal pressure; 4.4.2 Cylindrical pressure vessels; 4.4.3 Spherical pressure vessels; 4.4.4 Problems; 4.5 Saint-Venant's principle; Part II Beams and thin-wall structures5 Euler-Bernoulli Beam Theory; 5.1 The Euler-Bernoulli Assumptions; 5.2 Implications of the Euler-Bernoulli assumptions; 5.3 Stress resultants; 5.4 Beams subjected to axial loads; 5.4.1 Kinematic description; 5.4.2 Sectional constitutive law; 5.4.3 Equilibrium equations; 5.4.4 Governing equations; 5.4.5 The sectional axial stiffness; 5.4.6 The axial stress distribution; 5.4.7 Problems; 5.5 Beams subjected to transverse loads; 5.5.1 Kinematic description; 5.5.2 Sectional constitutive law; 5.5.3 Equilibrium equations; 5.5.4 Governing equations; 5.5.5 The sectional bending stiffness; 5.5.6 The axial stress distribution; 5.5.7 Rational design of beams under bending; 5.5.8 Problems; 5.6 Beams subjected to axial and transverse loads; 5.6.1 Kinematic description; 5.6.2 Sectional constitutive law; 5.6.3 Equilibrium equations; 5.6.4 Governing equations; 6 Three-Dimensional Beam Theory; 6.1 Kinematic description; 6.2 Sectional constitutive law; 6.3 Sectional equilibrium equations; 6.4 Governing equations; 6.5 Decoupling the three-dimensional problem; 6.5.1 Definition of the principal axes of bending; 6.5.2 Decoupled governing equations; 6.6 The principal centroidal axes of bending; 6.6.1 The bending stiffness ellipse; 6.7 Definition of the neutral axis; 6.8 Evaluation of sectional stiffnesses; 6.8.1 The parallel axis theorem; 6.8.2 Thin-walled sections; 6.8.3 Triangular area equivalence method; 6.8.4 Useful results; 6.8.5 Problems; 6.9 Summary of three-dimensional beam theory; 6.9.1 Examples; 6.9.2 Discussion of the results; 6.10 Problems; 7 Torsion; 7.1 Torsion of circular cylinders; 7.1.1 Kinematic description; 7.1.2 The stress field;7.1.3 Sectional constitutive law; 7.1.4 Equilibrium equations; 7.1.5 Governing equations; 7.1.6 The torsional stiffness; 7.1.7 Measuring the torsional stiffness; 7.1.8 The shear stress distribution; 7.1.9 Rational design of cylinders under torsion; 7.1.10 Problems; 7.2 Torsion combined with axial force or bending; 7.2.1 Problems; 7.3 Torsion of bars with arbitrary cross-sections; 7.3.1 Introduction; 7.3.2 Saint-Venant's solution; 7.3.3 Saint-Venant's solution for a rectangular cross-section; 7.3.4 Problems; 7.4 Torsion of a thin rectangular cross-section; 7.5 Torsion of thin-walled open sections; 7.5.1 Problems; 8 Thin-Walled Beams; 8.1 Basic equations for thin-walled beams; 8.1.1 The thin wall assumption; 8.1.2 Stress flows; 8.1.3 Stress resultants; 8.1.4 Local equilibrium equation; 8.2 Bending of thin-walled beams; 8.2.1 Problems; 8.3 Shearing of thin-walled beams; 8.3.1 Shearing of open sections; 8.3.2 Evaluation of stiffness static moments; 8.3.3 Shear flow distributions in open sections; 8.3.4 Problems; 8.3.5 Shear center for open sections; 8.3.6 Problems; 8.3.7 Shearing of closed sections; 8.3.8 Shearing of multi-cellular sections; 8.3.9 Problems; 8.4 The shear center; 8.4.1 Calculation of the shear center location; 8.4.2 Problems; 8.5 Torsion of thin-walled beams; 8.5.1 Torsion of open sections; 8.5.2 Torsion of closed section; 8.5.3 Comparison of open and closed sections; 8.5.4 Torsion of combined open and closed sections; 8.5.5 Torsion of multi-cellular sections; 8.5.6 Problems; 8.6 Coupled bending-torsion problems; 8.6.1 Problems; 8.7 Warping of thin-walled beams under torsion;8.7.1 Kinematic description; 8.7.2 Stress-strain relations; 8.7.3 Warping of open sections; 8.7.4 Problems; 8.7.5 Warping of closed sections; 8.7.6 Warping of multi-cellular sections; 8.8 Equivalence of the shear and twist centers; 8.9 Non-uniform torsion; 8.9.1 Non-uniform torsion: a classical approach; 8.9.2 Problems; 8.10 Structural idealization; 8.10.1 Lumping the thin-walled section into sheet and stringer components 8.10.2 Axial stress in the stringers; 8.10.3 Shear flow in the sheet components; 8.10.4 Torsion of sheet-stringer sections; 8.10.5 Problems; Part III Energy and variational methods9 Virtual Work Principles; 9.1 Introduction; 9.2 Equilibrium and work fundamentals; 9.2.1 Static equilibrium conditions; 9.2.2 Concept of mechanical work; 9.3 Principle of virtual work; 9.3.1 Principle of virtual work for a single particle; 9.3.2 Kinematically admissible virtual displacements; 9.3.3 Use of infinitesimals as virtual displacements; 9.3.4 Principle of virtual work for a system of particles; 9.3.5 Application of the principle of virtual work to mechanical systems; 9.3.6 Application of the principle of virtual work to trusses; 9.3.7 Generalized coordinates and forces; 9.3.8 Problems; 9.4 Principle of complementary virtual work; 9.4.1 Compatibility equations for a planar truss; 9.4.2 Principle of complementary virtual work for trusses; 9.4.3 Complementary virtual work; 9.4.4 Problems; 9.5 Unit load method for trusses; 9.5.1 Statement of the unit load method for trusses; 9.5.2 Application to trusses; 9.5.3 Problems .; 9.6 Unit load method for beams; 9.6.1 Beam deflection due to bending; 9.6.2 Beam deflection due to torsion; 9.6.3 Application to beam problems; 9.6.4 Deflections of beams with unsymmetric cross sections; 9.6.5 Problems; 9.7 Application of the unit load method to hyperstatic problems; 9.7.1 Force method for trusses; 9.7.2 Force method for beams; 9.7.3 Combined truss and beam problems; 9.7.4 Multiple redundancies; 9.7.5 Problems; 10 Energy Methods; 10.1 Conservative forces;10.1.1 Potential for internal and external forces; 10.1.2 Calculation of the potential functions; 10.2 Principle of minimum total potential energy;10.2.1 Nonconservative external forces; 10.3 Strain energy in springs; 10.3.1 Rectilinear springs; 10.3.2 Torsional springs; 10.4 Problems; 10.5 Strain energy in beams; 10.5.1 Beam under axial loads; 10.5.2 Beam under transverse loads;10.5.3 Beam under torsional loads; 10.6 Strain energy in solids; 10.6.1 General three-dimensional stress state; 10.6.2 Beams under multi-axis bending and axial load; 10.7 Applications to trusses; 10.7.1 Problems;10.7.2 Development of a finite element formulation for trusses;10.7.3 Problems;10.7.4 Applications to beams;10.8 Principle of minimum complementary energy;10.8.1 The potential of the prescribed displacements;10.8.2 Constitutive laws for elastic materials; 10.8.3 The principle of minimum complementary energy; 10.8.4 The principle of least work; 10.8.5 Examples using the PMCP/LWP; 10.8.6 Problems; 10.9 Energy theorems;10.9.1 Clapeyron's theorem; 10.9.2 Castigliano's first theorem; 10.9.3 Crotti-Engesser theorem; 10.9.4 Castigliano's second theorem; 10.9.5 Applications of energy theorems; 10.9.6 The dummy load method; 10.9.7 Unit load method revisited; 10.9.8 Conclusions; 10.9.9 Problems; 10.10Reciprocity theorems; 10.10.1Betti's theorem; 10.10.2Maxwell's theorem; 10.10.3Problems; 11 Variational and Approximate Solutions; 11.1 Approach; 11.2 Approximations based on the principle of minimum total potential energy; 11.2.1 Application to a bending of a beam; 11.2.2 Examples; 11.2.3 Problems; 11.3 The strong and weak statements of equilibrium; 11.3.1 The weak form for beams under axial loads; 11.3.2 Approximate solutions for beams under axial loads; 11.3.3 Problems; 11.3.4 The weak form for beams under transverse loads; 11.3.5 Approximate solutions for beams under transverse loads; 11.3.6 Problems 11.3.7 Equivalence with energy principles;11.3.8 The principle of minimum total potential energy; 11.3.9 Treatment of the boundary conditions; 11.4 Formal procedures for the derivation of approximate solutions; 11.4.1 Basic approximations; 11.4.2 Principle of virtual work; 11.4.3 The principle of minimum total potential energy; 11.4.4 Examples; 11.4.5 Problems; 11.5 A Finite Element formulation for beams; 11.5.1 Formulation of an Euler-Bernoulli beam element; 11.5.2 Examples; 11.5.3 Summary; 11.5.4 Problems; 12 Variational and Energy Principles; 12.1 Variational formulation of beam problems; 12.2 Mathematical Preliminaries; 12.2.1 Stationary point of a function; 12.2.2 Lagrange multiplier method; 12.2.3 Stationary point of a definite integral; 12.3 Variational and Energy Principles; 12.3.1 Review of the equations of linear elasticity; 12.3.2 The principle of virtual work;12.3.3 The principle of complementary virtual work; 12.3.4 The strain energy density function; 12.3.5 The stress energy density function; 12.3.6 The principle of minimum total potential energy; 12.3.7 The principle of minimum complementary energy; 12.3.8 Examples; 12.3.9 The principle of least work;12.3.10Hu-Washizu's principle; 12.3.11Hellinger-Reissner's principle; 12.3.12Problems; 12.4 Applications of Variational and Energy Principles; 12.4.1 The shear lag problem; 12.4.2 The non-uniform torsion problem; 12.4.3 The non-uniform torsion problem (closed sections); 12.4.4 The non-uniform torsion problem (open sections); 12.4.5 Problems; Part IV Advanced topics; 13 Introduction to Plasticity and Thermal Stresses; 13.1 Yielding under combined loading; 13.1.1 Introduction to yield criteria; 13.1.2 Tresca's criterion; 13.1.3 Von Mises' criterion; 13.1.4 Problems; 13.2 Applications of yield criteria to structural problems; 13.2.1 Problems; 13.2.2 Plastic bending; 13.2.3 Problems; 13.2.4 Plastic torsion; 13.2.5 Examples; 13.3 Thermal stresses in structures; 13.3.1 The direct method; 13.3.2 Examples; 13.3.3 Problems; 13.3.4 The constraint method; 13.4 Application to bars and trusses; 13.4.1 Examples; 13.4.2 Problems; 13.4.3 Application to beams; 13.4.4 Examples; 13.4.5 Problems; 14 Buckling of Beams; 14.1 Rigid bar with root torsional spring; 14.1.1 Analysis of a perfect system; 14.1.2 Analysis of an imperfect system; 14.2 Buckling of beams; 14.2.1 Equilibrium equations; 14.2.2 Buckling of a pinned-pinned beam (Equilibrium approach); 14.2.3 Buckling of a pinned-pinned beam (Imperfection approach); 14.2.4 Work done by the axial force; 14.2.5 Buckling of a pinned-pinned beam (Energy approach); 14.2.6 Examples; 14.2.7 Buckling of beams with various end conditions; 14.2.8 Problems; 14.3 Buckling of sandwich beams; 15 Shearing Deformations in Beams; 15.1 Introduction; 15.1.1 A simplified approach; 15.1.2 An equilibrium approach; 15.1.3 Examples; 15.1.4 Problems; 15.2 Shear deformable beams: an energy approach; 15.2.1 Shearing effects on static deflections; 15.2.2 Examples; 15.2.3 Shearing effects on buckling; 15.2.4 Shearing and rotary inertia effects on vibration; 15.2.5 Problems; 16 Kirchhoff Plate Theory; 16.1 Governing equations of Kirchhoff plate theory; 16.1.1 Kirchhoff assumptions; 16.1.2 Stress resultant; 16.1.3 Equilibrium equations; 16.1.4 Constitutive laws; 16.1.5 Summary of Kirchhoff plate theory; 16.2 The bending problem; 16.2.1 Typical boundary conditions; 16.2.2 Simple plate bending solutions; 16.2.3 Problems; 16.3 Anisotropic plates; 16.3.1 Laminated composite plates; 16.3.2 Constitutive laws for laminated composite plates; 16.3.3 The in-plane stiffness matrix; 16.3.4 Problems; 16.3.5 The bending stiffness matrix; 16.3.6 The coupling stiffness matrix; 16.3.7 Problems; 16.3.8 Directionally stiffened plates; 16.3.9 Governing equations for anisotropic plates; 16.4 Solution techniques for rectangular plates; 16.4.1 Navier's solution for simply supported plates; 16.4.2 Examples; 16.4.3 Problems; 16.4.4 Levy's solution; 16.4.5 Problems; 16.5 Circular plates; 16.5.1 Governing equations for the bending of circular plates; 16.5.2 Circular plates subjected to loading presenting circular symmetry; 16.5.3 Examples; 16.5.4 Problems; 16.5.5 Circular plates subjected to arbitrary loading; 16.5.6 Examples;;16.5.7 Problems 16.6 Energy formulation of Kirchhoff plate theory; 16.6.1 The virtual work done by internal forces and moments; 16.6.2 The virtual work done by the applied loads; 16.6.3 The principle of virtual work for Kirchhoff plates; 16.6.4 The principle of minimum total potential energy for Kirchhoff plates; 16.6.5 Energy based approximate solutions for Kirchhoff plates; 16.6.6 Examples;16.6.7 Problems; 16.7 Shear deformable plates; 16.7.1 Problems;16.8 Buckling of plates; 16.8.1 Problems; 17 Appendix: Mathematical Tools;17.1 Coordinate systems and transformations; 17.1.1 The rotation matrix; 17.1.2 Rotation of vector components; 17.1.3 The rotation matrix in two dimensions; 17.1.4 Rotation of vector components in two dimensions; 17.2 Least-square solution of linear systems with redundant equations; 17.3 Arrays and matrices; 17.3.1 Partial derivatives of a linear form; 17.3.2 Partial derivatives of a quadratic form; 17.4 Orthogonality properties of trigonometric functions; References; Index
£58.49
United Nations European Global Navigation Satellite System and
Book SynopsisThis report investigates how European Union space technologies support the fulfilment of the SDGs. It has been jointly prepared by the United Nations Office for Outer Space Affairs (UNOOSA) - in charge of promoting international cooperation in the peaceful use and exploration of space, and in the utilization of space science and technology for sustainable economic and social development - and the European GNSS Agency (GSA), which is the European Union agency operating EGNOS and Galileo and is in charge of ensuring the maximization of socioeconomic benefits from the use of the European Union satellite navigation systems. The analysis shows that all the SDGs are positively impacted by the benefits stemming from the use of European Global Navigation Satellite Systems (EGNSS) and Copernicus applications and, out of the 169 indicators associated, 65 (almost 40 per cent) directly benefit from using the EGNSS and Copernicus services, either helping monitor the status of achievement of a given SDG or actively contributing to its fulfilment
£33.96
PHI Learning Helicopter Aerodynamics
Book SynopsisThis book is developed to serve as a concise text for a course on helicopter aerodynamics at the introductory level. It introduces to the rotary-wing aerodynamics, with applications to helicopters, and application of the relevant principles to the aerodynamic design of a helicopter rotor and its blades. The basic aim of this book is to make a complete text covering both the basic and applied aspects of theory of rotary wing flying machine for students, engineers, and applied physicists.The philosophy followed in this book is that the subject of helicopter aerodynamics is covered combining the theoretical analysis, physical features and the application aspects. Considerable number of solved examples and exercise problems with answers are coined for this book. This book will cater to the requirement of numerical problems on helicopter flight performance, which is required for the students of aeronautical/aerospace engineering.SALIENT FEATURES: To provide an introductory treatment of the aerodynamic theory of rotary-wing aircraft To study the fundamentals of rotor aerodynamics for rotorcraft in hovering flight, axial flight, and forward flight modes To perform blade element analysis, investigate rotating blade motion, and quantify basic helicopter performance
£20.57
New India Publishing Agency Electric Machines in Agriculture:
Book Synopsis
£171.12
New India Publishing Agency Engendering Agricultural Development: Dimensions
Book Synopsis
£209.90
Lanasta The Legendary Douglas DC-3: A Pictorial Tribute
Book SynopsisFollowing on from the epoch-making DC-2 technology, the DC-3 is generally considered the greatest single commercial transport plane in history, and certainly the most famous. Indeed, the DC-3 revolutionized air travel to an extent not equaled until the arrival of the jet age. Many of these revolutions related to safety; thanks to the DC-3’s reputation for reliability, air travel insurance finally became available to the general public in 1937. This is the airliner that not only made flying respectable but enabled the emerging aviation industry to end its reliance on mail subsidies and profit from passenger journeys. DC-3 is still flying eight decades after their first debut - this book is a tribute to its brilliant design.Trade Review'... een zeer kleurrijk boek. (...) Het boek is een prachtig eerbetoon en een mooie momentopname van wat er op dit moment op de wereld nog te zien is van dit ontwerp van voor de Tweede Wereldoorlog.' – De Vliegende Hollander
£35.14
Springer Verlag, Singapore Formal Methods for Safety and Security: Case
Book SynopsisThis volume is the outcome of deliberations on formal methods in aerospace. The book specially delves into the use of formal methods for verification, validation, and optimization of software in safety critical and time critical applications, such as those in aerospace engineering. The chapters in this book are authored by leading corporate and government R&D scientists. The contents of this book will be useful to researchers and professionals alike. Table of ContentsFormal Methods – A Need for Practical Applications.- Formal Methods & Tools for Safety of Critical Systems.- Taming the Enemy: Framework for Comparative Analysis of Safe String Libraries.- Dynamic Constrained Objects for Vehicular Network Modeling.- Adoption of Formal Methods in Software Safety Analysis.- Model-Based Safety Validation for Embedded Real-Time Systems.- Arguing formally about Flight Controls using SLDV and NuSMV.- Formal Methods: Techniques, Applications, Thrust Areas and Future Prospects.- Design Fault Identification in Model-Based Design (MBD) for Safety Critical Systems.- Formal Methods Workflow for Model Based Development.- Race that never ends!.
£89.99
Springer Verlag, Singapore Development of Navigation Technology for Flight Safety
Book SynopsisThis book highlights practical solutions for flight safety improvement techniques, which are currently the focus of the International Civil Aviation Organization (ICAO). It has become clear that, in order to rapidly and significantly improve flight safety, the integrated use of new aeronautical technologies is called for. Considering the size of the aviation fleet, its constant growth and the long service lives of aircraft, new technologies should be adapted both to cutting-edge air navigation systems and to those that have been used for over a decade. Concretely, the book discusses methodological approaches to the construction of ground and on-board avionics that make it possible to achieve improved flight safety using innovative new methods. The proposed approaches are illustrated with real-world examples of e.g. satellite-based navigation systems and enhanced ground proximity warning systems. The book is written for professionals involved in the development of avionics systems, as well as students, researchers and experts in the field of radiolocation, radio navigation and air traffic control, the book will support the development and modeling of radio technical complexes, as well as the analysis of complex radio technical systems.Table of ContentsGENERAL DESCRIPTION OF FLIGHT SAFETY PROBLEMS Analysis of the state and prospects for the development of instrument landing systems and collision avoidance systems Features of global navigation satellite systems as an instrument basis for improving flight safety Augmentations – the main method to improve the performance characteristics of global navigation satellite systems Analysis of requirements for satellite-based landing systems and collision avoidance systems General methods and techniques to improve flight efficiency and safety when using satellite-based landing systems and collision avoidance systems Flight safety indicators Conclusions to Chapter 1 METHODOLOGY FOR CONSTRUCTING SATELLITE-BASED LANDING SYSTEMS AND COLLISION AVOIDANCE SYSTEMS Theoretical background of a formalized methodological approach to the selection of basic elements for radio-electronic complexes to improve flight efficiency and safety Methods for building the structure of the ground and onboard radio-electronic complexes of satellite-based landing systems with augmentations of global navigation satellite systems Methods and rules for the development of a collision avoidance system with the use of global navigation satellite system technologies Directions and methods to enhance satellite-based landing systems and collision avoidance systems Conclusions to Chapter 2 METHODS FOR IMPROVING FLIGHT EFFICIENCY AND SAFETY FOR SATELLITE-BASED LANDING SYSTEMS Method for increasing the accuracy and integrity of the guidance signals based on the construction and use of volumetric distribution diagrams for radio waves multipath errors and the system structure for its implementation Method for ensuring integrity and continuity of guidance signals based on the use of an integrated signal-to-noise ratio for pseudoranges in presence of radiointerference Method for increasing accuracy and integrity of guidance signals based on pseudorange error compensation using phase measurements and the structure of the radioelectronic complex for its implementation Method for increasing accuracy, integrity, continuity and availability of guidance signals based on the use of pseudo-satellite signals and the system structure for its implementation Conclusions to Chapter 3 METHODS FOR IMPROVING FLIGHT EFFICIENCY AND SAFETY BASED ON TECHNOLOGIES APPLICABLE IN COLLISION AVOIDANCE SYSTEMS Method for improving flight safety by generating a warning about a potential collision based on the three-dimensional synthesis of the underlying surface sections and the display of hazardous elements Method for increasing the flight effectiveness and safety by assessing the possibility of vertical maneuvering and determining the direction of the turn Method for increasing the flight effectiveness and safety by identifying hazardous terrain, taking into account the possibility of a reverse turn, and the system structure for its implementation Method for improving flight efficiency and safety by analyzing the space inside a corridor safe for flight Conclusions to Chapter 4 INTEGRATED TECHNICAL SOLUTIONS ON THE JOINT USE OF TECHNOLOGIES APPLICABLE IN COLLISION AVOIDANCE SYSTEMS AND SATELLITE-BASED LANDING SYSTEMS Principles of constructing an integrated flight safety enhancement system based on the collision avoidance system and the satellite-based landing system Method for preventing aircraft landings on an unauthorized runway by calculating a virtual glide path Method for notifying of the aircraft or UAV position during the landing and roll-on operation Assessment of flight safety and efficiency improvements with the use of integrated systems Conclusions to Chapter 5 RECOMMENDATIONS FOR THE APPLICATION OF THE PROPOSED TECHNICAL SOLUTIONS IN THE SATELLITE-BASED LANDING SYSTEMS AND COLLISION AVOIDANCE SYSTEMS Principles of construction and design features of onboard equipment to improve flight efficiency and safety Construction of an onboard navigation and landing complex on the basis of the satellite-based landing system and the collision avoidance system Results of the satellite-based landing system flight tests Results of the Enhanced Ground Proximity Warning System flight tests and operation Conclusions to Chapter 6 CONCLUSIONs REFERENCES
£67.49
Springer Verlag, Singapore Conditional Function Control of Aircraft
Book SynopsisThis book highlights the prevention of possible accidents and crashes of aircrafts by analyzing the many factors that affect such events. It includes the theoretical study of known ideas and concepts, as well as a set of new methods and mathematical models. It contains factual information to investigate famous disasters and aviation accidents with aircrafts. The book proposes methods and models that can be the basis in developing guidance material for decision-making by the flight crew and experts in air traffic control. Some of the contents presented in this book are also useful in the design and operation of data transmission systems of aircraft. The book is intended for engineering and technical specialists engaged in the development, manufacturing and operations of onboard radio electronic systems of aircraft and ground-based radio engineering support for flights, as well as graduate students and senior students of radio engineering specialties. It is useful to researchers and managers whose activities are related to air traffic control.Table of ContentsIntroduction 1. Analysis of the state of the problem of modeling functioning ergatic air traffic management information system 1.1. The state of the security problem and traffic management aircraft in the area of the aerodrome 1.2. A modern approach to the systematic dynamic description of the functioning of an ergatic system 1.3. Set-theoretic model of information interaction of the elements of the ergatic information system of air traffic control 1.4. Presentation of informational interaction ergatic elements in an ergatic information system 1.5. Logical-linguistic model for choosing an analytical model parry adverse effects for ergatic elements 1.6. Synthesis of decision-making procedural model for an ergatic element during air traffic flow arrangement 1.7. The method of synthesis of models for the representation of ergatic elements in an ergatic information system References 2. The methodology of functional control of the aircraft and parrying special situations 2.1. Analysis of aircraft failures and malfunctions by aviation systems and groups of factors of causes 2.2. Decision-making model for parrying special situations on board an aircraft 2.3. Methods of functional monitoring of the state of the aircraft and the organization of information support for decision-making in special situations 2.4. A model of the functioning of the information support system for decision-making of the aircraft crew in a particular situation References 3. The architecture of the safety system in the airspace of the Russian Federation 3.1. The role and place of the decision-support information system in the structure of the ergatic system “aircraft - crew,” “aircraft - operator of an unmanned aerial vehicle.” 3.2. Development of the architecture of a safety system in the airspace of the Russian Federation 3.3. A model for the optimal placement of critical information entities in a unified safety system 3.4. The concept of the creation and development of the Air Navigation System of Russia References 4. The mathematical model for building a conflict-free flow of aircraft in the zone of responsibility of the officer of the near zone 4.1. Features of information support during the formation of the flow of aircraft during approach 4.2. Justification of the need to develop a method and models for organizing information support for the officer of the near zone in the detection and resolution of potential conflict situations 4.3. Definition of space and formation trajectories Conflict-free aircraft flow during an approach 4.4. A model for constructing an aircraft delay maneuver for a given interval 4.5. The method of organizing information support for the near zone officer in the detection and resolution of potential conflict situations 4.5.1. Description of the method of organizing information support for the near zone when detecting and resolving potential conflict situations between aircraft approaching 4.5.2. Organization of information support for the near zone officer when forming the queue of aircraft without a priority of service 4.5.3. Organization of information support for the near zone officer when forming a queue of aircraft with a priority of service for an incoming aircraft 4.5.4. Organization of information support for the near zone officer in the formation of the aircraft queue with the priority of service and taking into account fuel residues onboard each aircraft References 5. Formation of solutions for optimizing the activities of the landing zone officer 5.1. Building a model of a guaranteed aircraft landing approach 5.2. Defining a set of safe approach paths 5.3. Determining the optimal safe approach path 5.4. A mathematical model for constructing an optimal approach path 5.4.1. The principle of maximum performance in solving the problem of parrying deviations from the landing course 5.4.2. Aircraft movement model during a landing approach with a decrease in speed and two turns 5.4.3. Aircraft Double U-Turn Modeling 5.5. Development of a set of problem-oriented programs and evaluation confidence modeling 5.6. Assessment of the complexity of the algorithmic support system decision-making workstation of the landing zone officer 5.7. Construction of the approach zone and recommendations to the zone leader aircraft control landing using a decision support system 5.8. Acceptance Support System Software Development solutions for the automated workplace of the landing zone officer 5.9. Estimation of the reliability of the model for constructing an optimal approach trajectory for landing 5.10. Development of the technology for the operation of service dispatchers air traffic (flight control) during flights in special conditions and exceptional cases in flight References
£80.99
Springer Verlag, Singapore Footprints in Cambridge and Aviation Industries
Book SynopsisThe book is a collection of academician Yanzhong Zhang’s research papers published in English. It represents the development of aerospace systems engineering and information technology in China over the past 4 decades. Regarded as the crucial reference materials of related disciplines, it falls into three categories, namely, information technique, aeronautical engineering strategy issue of development, as well as PhD thesis.Table of ContentsInformation Technique.- Aeronautical Engineering.- Strategy Issue of Development.- Ph.D. Thesis.
£161.99
Springer Verlag, Singapore Adaptive Compensation of Nonlinear Actuators for
Book SynopsisThis book provides a basic understanding of adaptive control and its applications in Flight control. It discusses the designing of an adaptive feedback control system and analyzes this for flight control of linear and nonlinear aircraft models using synthetic jet actuators. It also discusses control methodologies and the application of control techniques which will help practicing flight control and active flow control researchers. It also covers modelling and control designs which will also benefit researchers from the background of fluid mechanics and health management of actuation systems.The unique feature of this book is characterization of synthetic jet actuator nonlinearities over a wide range of angles of attack, an adaptive compensation scheme for such nonlinearities, and a systematic framework for feedback control of aircraft dynamics with synthetic jet actuators.Table of ContentsIntroduction.- Active Flow Control.- Adaptive Compensation at Low Angles of Attack: Linear Aircraft Model.- Adaptive Compensation at Low Angles of Attack: Nonlinear Aircraft Model.- Adaptive Compensation at High Angles of Attack.- Adaptive Compensation of Signal-Dependent Actuator Nonlinearities.- High-Order Design of Adaptive Inverses for Signal-Dependent Actuator Nonlinearities.- Adaptive Synthetic Jet Actuation for Aircraft Control.- Adaptive Actuator Fault Diagnosis in Uncertain Systems.- Adaptive Sensor Fault Diagnosis in Uncertain Systems.- Integrated Adaptive Diagnostics and Control.
£107.99
Springer Verlag, Singapore China's Space Programme: From the Era of Mao
Book SynopsisThis book comprehensively covers the history and current developments of space programme of China. It presents the complete story of China’s space programme from its origins through to present day activities on the International Space Station. This monograph further discusses the role of China’s space strategy in its emergence as a major power on the world stage. The book also presents the context of China’s space program within the larger narrative of international space development. The book binds together the diverse political, military, economic and technology aspects into a coherent understanding and explains their role in the establishment and growth of Chinese space programme. Given the contents, this book will be a valuable source of information for students, researchers, and historians in the area of space studies.Trade Review“China’s Space Programme: From the Era of Mao Zedong to Xi Jinping by S Chandrashekhar provides a detailed account of the country’s rise to become a space power worth reckoning. … Each chapter carries a wealth of information in the form of tables and diagrams. … The richness of information on the Chinese Space programme makes the book a historical study, a tutorial, a study in management, and a reference guide.” (Arup Dasgupta, Geospatial Artha, Vol. 1 (5), January-February, 2023)Table of ContentsThe Origins of China’s Space Programme.- Economic Reform and the Deng Era.- New Challenges to the Space Programme.- The Growth Phase of China’s Space Programme.- Strategic Trends and Future Directions.- Chinese Recoverable Satellites.- China’s Communications Satellites.- China’s Weather Satellites.- Remote Sensing Satellites.- China’s Navigation Satellite Constellation.- The Human Space Flight Programme.- Breakthrough Research in Space Science and Applications.- China’s Military Satellites.
£28.49
Springer Verlag, Singapore China's Space Programme: From the Era of Mao
Book SynopsisThis book comprehensively covers the history and current developments of space programme of China. It presents the complete story of China’s space programme from its origins through to present day activities on the International Space Station. This monograph further discusses the role of China’s space strategy in its emergence as a major power on the world stage. The book also presents the context of China’s space program within the larger narrative of international space development. The book binds together the diverse political, military, economic and technology aspects into a coherent understanding and explains their role in the establishment and growth of Chinese space programme. Given the contents, this book will be a valuable source of information for students, researchers, and historians in the area of space studies.Trade Review“China’s Space Programme: From the Era of Mao Zedong to Xi Jinping by S Chandrashekhar provides a detailed account of the country’s rise to become a space power worth reckoning. … Each chapter carries a wealth of information in the form of tables and diagrams. … The richness of information on the Chinese Space programme makes the book a historical study, a tutorial, a study in management, and a reference guide.” (Arup Dasgupta, Geospatial Artha, Vol. 1 (5), January-February, 2023)Table of ContentsThe Origins of China’s Space Programme.- Economic Reform and the Deng Era.- New Challenges to the Space Programme.- The Growth Phase of China’s Space Programme.- Strategic Trends and Future Directions.- Chinese Recoverable Satellites.- China’s Communications Satellites.- China’s Weather Satellites.- Remote Sensing Satellites.- China’s Navigation Satellite Constellation.- The Human Space Flight Programme.- Breakthrough Research in Space Science and Applications.- China’s Military Satellites.
£28.49
Springer Verlag, Singapore Unmanned Aerial Systems in Precision Agriculture:
Book SynopsisThis book, consisting of 8 chapters, describes the state-of-the-art technological progress and applications of unmanned aerial vehicles (UAVs) in precision agriculture. It focuses on the UAV application in agriculture, such as crop disease detection, mid-season yield estimation, crop nutrient status, and high-throughput phenotyping. Different from individual papers focusing on a specific application, this book provides a holistic view for readers with a wide range of subjects. In addition to researchers in the areas of plant science, plant pathology, breeding, engineering, it is also intended for undergraduates and graduates who are interested in imaging processing, artificial intelligence in agriculture, precision agriculture, agricultural automation, and robotics.Table of ContentsApplications of UAVs and machine learning in agriculture.- Robot Operating System Powered Data Acquisition for Unmanned Aircraft Systems in Digital Agriculture.- Unmanned aerial vehicle (UAV) applications in cotton production.- Time effect after initial wheat lodging on plot lodging ratio detection using UAV imagery and deep learning.- UAV mission height effects on wheat lodging ratio detection.- Wheat-Net: An Automatic Dense Wheat Spike Segmentation Method Based on An Optimized Hybrid Task Cascade Model.- UAV multispectral remote sensing for yellow rust mapping: opportunities and challenges.- Corn Goss's Wilt disease assessment based on UAV imagery.
£134.99
Springer Verlag, Singapore Aerodynamics
Book SynopsisThis textbook highlights the fundamentals of aerodynamics and the applications in aeronautics. The textbook is divided into two parts: basic aerodynamics and applied aerodynamics. The first part focuses on the basic principles and methods of aerodynamics. The second part covers the aerodynamic characteristics of aircraft in low speed, subsonic, transonic and supersonic flows. The combination of the two parts aims to cultivate students' aerospace awareness, build the ability to raise and solve problems and the ability to make comprehensive use of the knowledge to carry out innovative practice. This book is intended for undergraduates majoring in aircraft design and engineering, engineering mechanics, flight mechanics, missile design, etc. It can also be used as a reference for postgraduates, researchers and engineers of aerospace related majors.Table of ContentsPart 1 Fundamentals of Aerodynamics Chapter 1. Introduction Chapter 2. Basic Properties of Fluid and Hydrostatics Chapter 3. Fundamentals of Fluid Kinematics and Dynamics Chapter 4 .Plane Potential Flow of Ideal Incompressible Fluid Chapter 5. Fundamentals of Viscous Fluid Dynamics Chapter 6. Boundary Layer Theory and its Approximation Chapter 7. Fundamentals of Compressible Aerodynamics Part 2 Applied Aerodynamics Chapter 8. Flow and Aerodynamic Characteristics of Low Speed Airfoil Chapter 9. Aerodynamic Characteristics of Low Speed Wing Flow Chapter 10. Aerodynamic Characteristics of Low Speed Fuselage Wing Body Combination Chapter 11. Aerodynamic Characteristics of Subsonic Thin Airfoils and Wings Chapter 12. Aerodynamic Characteristics of Supersonic Thin Airfoils and Wings Chapter 13. Aerodynamic Characteristics of Transonic Thin Airfoils and Wings Chapter 14. High Lift Device and Its Aerodynamic Performance
£66.49
Springer Verlag, Singapore Advances in Guidance, Navigation and Control:
Book SynopsisThis book features the latest theoretical results and techniques in the field of guidance, navigation, and control (GNC) of vehicles and aircrafts. It covers a wide range of topics, including but not limited to, intelligent computing communication and control; new methods of navigation, estimation and tracking; control of multiple moving objects; manned and autonomous unmanned systems; guidance, navigation and control of miniature aircraft; and sensor systems for guidance, navigation and control etc.Presenting recent advances in the form of illustrations, tables, and text, it also provides detailed information of a number of the studies, to offer readers insights for their own research. In addition, the book addresses fundamental concepts and studies in the development of GNC, making it a valuable resource for both beginners and researchers wanting to further their understanding of guidance, navigation, and control.Table of ContentsA Survey of Relative Motion Dynamics and Control of Distributed Satellite Formation.- Determination Technology and Accuracy Analysis of Configuration Parameters of Ground System Dual Satellite Formation Based on Navigation Data.- UAV path planning based on improved GWO algorithm.- A Review on tracking control of the underactuated vessel with time delays.- A Multimodal Image Matching Algorithm Based on Structure Feature.- Full-scale Attitude Solution Based on Dual Euler Method.- Q-Learning Based Online Adaptive Flight Control for Fixed-Wing UAV.
£427.49
Springer Verlag, Singapore Key Basic Scientific Problems on Near-Space
Book SynopsisThis book mainly introduces the research overview, research results, and follow-up prospects of “Key Basic Scientific Problems on Near-Space Vehicles”, a major research plan of National Natural Science Foundation of China (hereinafter referred to as the Plan). The Plan is the first systematic basic hypersonic research program in China. From its inception in 2007 to its successful completion in 2016, the Plan lasted nine years, funded a total of 173 projects, and the funding totaled 190 million yuan. From the perspective of major national needs and scientific discipline development, the book focuses on four key scientific issues: aerodynamics in a near-space flight environment; advanced propulsion theories and methods; ultralight materials/structures, thermal environment prediction and thermal protection; and intelligent autonomous control theories and methods for hypersonic vehicles. The book also demonstrates China’s systematic and innovative achievements in interdisciplinary theories and methods and innovative techniques, paving the way for a distinctively Chinese basic research framework and further breakthroughs of near-space hypersonic vehicles.Table of ContentsProject Overview.- Research Status at Home and Abroad.- Major Research Achievements.- Outlook.
£104.49
Springer Analytical Dynamics of Nonlinear Rotors
Book SynopsisIntroduction.- Analytical Methods for Periodic Motions.- Periodic Solutions for Buckled Nonlinear Jeffcott Rotors.- Semi-analytic Solutions of Periodic Motions in Nonlinear Jeffcott Rotors.- Modeling for Journal Bearing Rotors.
£142.49
Springer Verlag, Singapore Fault Tolerant Control of Large Civil Aircraft
Book SynopsisThis book provides a comprehensive analysis of fault tolerant control (FTC) for more-electric civil aircraft. The book's major highlight is its comprehensive and systematic approach to FTC design, making it an ideal resource for readers interested in learning about FTC design for civil aircraft.
£103.50
Springer Solar Thermal Thruster
Book Synopsis
£40.49
Independently Published Aerodynamics for the Commercial Pilot
Book SynopsisDespite aircraft coming in many shapes and sizes, they all utilize the same basic aerodynamic principles that have not changed much since the early days of flight. Whether you are a new pilot that is exploring aerodynamics in greater detail, or a commercial pilot who has been flying for countless years, it is essential to understand the aerodynamics of flight.From the author of the hugely popular Principles of Flight for the Private Pilot, this book takes the reader deeper into the world of aerodynamics. This book follows closely the syllabi of Aerodynamics for the Commercial Pilot from a range of aviation authorities around the world, with a particular focus on practical aviation, thereby linking science with the real world.
£17.09
