Description

Book Synopsis


Table of Contents
Part A: Fundamentals of Structural Analysis Section A1: Elasticity 1. Basic elasticity 2. Two-dimensional problems in elasticity 3. Torsion of solid sections Section A2: Virtual work, energy, and matrix methods 4. Virtual work and energy methods 5. Energy methods 6. Matrix methods Section A3: Thin plate theory 7. Bending of thin plates Section A4: Structural instability 8. Columns 9. Thin plates Section A5: Vibration of structures 10. Structural vibration Part B: Analysis of Aircraft Structures Section B1: Principles of stressed skin construction 11. Materials 12. Structural components of aircraft Section B2: Airworthiness and airframe loads 13. Airworthiness 14. Airframe loads 15. Fatigue Section B3: Bending, shear and torsion of thin-walled beams 16. Bending of open and closed, thin-walled beams 17. Shear of beams 18. Torsion of beams 19. Combined open and closed section beams 20. Structural idealization Section B4: Stress analysis of aircraft components 21. Wing spars and box beams 22. Fuselages 23. Wings 24. Fuselage frames and wing ribs 25. Laminated composite structures Section B5: Structural and loading discontinuities 26. Closed section beams 27. Open section beams Section B6: Introduction to aeroelasticity 28. Wing problems

Aircraft Structures for Engineering Students

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    A Paperback / softback by T.H.G. Megson

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      Publisher: Elsevier - Health Sciences Division
      Publication Date: 22/09/2021
      ISBN13: 9780128228685, 978-0128228685
      ISBN10: 0128228687

      Description

      Book Synopsis


      Table of Contents
      Part A: Fundamentals of Structural Analysis Section A1: Elasticity 1. Basic elasticity 2. Two-dimensional problems in elasticity 3. Torsion of solid sections Section A2: Virtual work, energy, and matrix methods 4. Virtual work and energy methods 5. Energy methods 6. Matrix methods Section A3: Thin plate theory 7. Bending of thin plates Section A4: Structural instability 8. Columns 9. Thin plates Section A5: Vibration of structures 10. Structural vibration Part B: Analysis of Aircraft Structures Section B1: Principles of stressed skin construction 11. Materials 12. Structural components of aircraft Section B2: Airworthiness and airframe loads 13. Airworthiness 14. Airframe loads 15. Fatigue Section B3: Bending, shear and torsion of thin-walled beams 16. Bending of open and closed, thin-walled beams 17. Shear of beams 18. Torsion of beams 19. Combined open and closed section beams 20. Structural idealization Section B4: Stress analysis of aircraft components 21. Wing spars and box beams 22. Fuselages 23. Wings 24. Fuselage frames and wing ribs 25. Laminated composite structures Section B5: Structural and loading discontinuities 26. Closed section beams 27. Open section beams Section B6: Introduction to aeroelasticity 28. Wing problems

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