Search results for ""Author Darrol Stinton""

The new edition of this classic textbook, used by universities, training schools, industry and enthusiasts, has been extended to feature a number of new studies in practical aeroplane design. Mathematics - which general readers may skip - is the minimum needed to work out common sense shapes, aimed at meeting the certification requirements of the three world airworthiness authorities: FAA (USA), British CAA and European JAA. Land and seaplanes are included, from microlight and commuter, to a 30-seat surface-effect (ekranoplan) regional transport, to satisfy specific markets. A new chapter, on "Using the back of an envelope", shows how to make "ballpark" technical judgements. Darrol Stinton MBE, PhD, CEng, FRAeS, FRINA, MIMechE, RAF(Retd) was born in New Zealand and grew up in England. He is qualified test pilot and aeronautical engineer who worked in the design offices of the Blackburn and De Havilland aircraft companies before joining the RAF. His test flying spanned 35 years and more than 340 types of aircraft, first as an experimental test pilot at Farnborough; then 20 years as airworthiness certification test pilot for the UK Civil Aviation Authority on light aeroplanes and seaplanes, before turning freelance. He has lectured regularly at the Empire Test Pilots' School, Loughborough University, the Royal Aeronautical Society (of which he is pas Vice President), and the Royal Institution of Naval Architects. His company specializes in cross-fertilization between aircraft and marine craft design and operation.

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The Anatomy of the Aeroplane is the first of a trilogy of textbooks, including The Design of the Aeroplane and Flying Qualities and Flight Testing of the Aeroplane, which have been described internationally as classics and required reading for professionals and students of aeronautics around the world. Together, they link theory and practical experience in the areas of aeronautical form and function, design, flying qualities and flight testing. The Anatomy concentrates on a broad landscape of physical principles and technological advances, among aeroplanes designed to meet specific operational requirements, from military strike to disaster relief. The new edition has been extensively updated since its first publication in 1966. It discusses critically the advantages and disadvantages of different subsonic and supersonic aerodynamic, propulsive and structural configurations of light to heavy aircraft; stealth technology; design for operation in surface (ground) effect; and fly-by-wire, fly-by-light and high-order control systems to achieve extreme agility. It is extensively illustrated with additional plates and drawings.

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