Aircraft Performance

Aircraft Performance

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Zusammenfassung

This book describes the principles and equations required for evaluating the performance of an aircraft. The greater part of the book refers to subsonic aircraft flying at subcritical speeds, which can be dealt with using relatively simple equations, but it is shown that much of this simplicity is also valid for transonic and supersonic speeds.

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Aircraft Performance by W Austyn Mair

This book describes the principles and equations required for evaluating the performance of an aircraft. After introductory chapters on the atmosphere, basic flight theory and drag, the book goes on to consider in detail the estimation of climbing performance, the relevant characteristics of power plants, take-off and landing performance, range and turning performance. There is then a short account of the use of vectored thrust and a final chapter on transonic and supersonic flight. The emphasis is on deriving and applying simple analytical expressions rather than on computations from extensive numerical data, but all the exemplary calculations refer to current types of aircraft and the few necessary data are provided. The greater part of the book refers to subsonic aircraft flying at subcritical speeds, which can be dealt with using relatively simple equations, but it is shown that some of this simplicity can be carried over to transonic and supersonic speeds.
Review of the hardback: 'What a pleasure it is to welcome a book on performance which has all the necessary virtuesIt sets sensible boundaries and inside them it is comprehensive, well balanced and well written.' Aeronautical Journal
SKU Nicht verfügbar
ISBN 13 9780521568364
ISBN 10 0521568366
Titel Aircraft Performance
Autor W Austyn Mair
Serie Cambridge Aerospace Series
Buchzustand Nicht verfügbar
Bindungsart Paperback
Verlag Cambridge University Press
Erscheinungsjahr 1996-03-14
Seitenanzahl 324
Hinweis auf dem Einband Die Abbildung des Buches dient nur Illustrationszwecken, die tatsächliche Bindung, das Cover und die Auflage können sich davon unterscheiden.
Hinweis Nicht verfügbar