Sprache: Englisch
Verlag: Cambridge University Press, 1996
ISBN 10: 0521568366 ISBN 13: 9780521568364
Anbieter: Anybook.com, Lincoln, Vereinigtes Königreich
EUR 28,09
Anzahl: 1 verfügbar
In den WarenkorbZustand: Fair. This is an ex-library book and may have the usual library/used-book markings inside.This book has soft covers. Clean from markings. In fair condition, suitable as a study copy. Please note the Image in this listing is a stock photo and may not match the covers of the actual item,550grams, ISBN:9780521568364.
Sprache: Englisch
Verlag: Cambridge University Press, 1996
ISBN 10: 0521568366 ISBN 13: 9780521568364
Anbieter: Ria Christie Collections, Uxbridge, Vereinigtes Königreich
EUR 81,40
Anzahl: Mehr als 20 verfügbar
In den WarenkorbZustand: New. In.
Sprache: Englisch
Verlag: Cambridge University Press, 1996
ISBN 10: 0521568366 ISBN 13: 9780521568364
Anbieter: Kennys Bookstore, Olney, MD, USA
EUR 148,09
Anzahl: Mehr als 20 verfügbar
In den WarenkorbZustand: New. Describes the principles and equations required for evaluating the performance of an aircraft. Series: Cambridge Aerospace Series. Num Pages: 324 pages, 120 b/w illus. BIC Classification: TGMF1; TRP. Category: (P) Professional & Vocational. Dimension: 228 x 152 x 18. Weight in Grams: 480. . 2008. Reprint. paperback. . . . . Books ship from the US and Ireland.
Sprache: Englisch
Verlag: Cambridge University Press, 1996
ISBN 10: 0521568366 ISBN 13: 9780521568364
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Taschenbuch. Zustand: Neu. Druck auf Anfrage Neuware - Printed after ordering - 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.