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Aircraft Dynamic Stability and Response: Pergamon International Library of Science, Technology, Engineering and Social Studies - Couverture souple

 
9780080247687: Aircraft Dynamic Stability and Response: Pergamon International Library of Science, Technology, Engineering and Social Studies

Synopsis

Aircraft Dynamic Stability and Response deals with the fundamentals of dynamic stability in aircraft. Topics covered include flight dynamics, equations of motion, and lateral and longitudinal aerodynamic derivatives. Basic lateral and longitudinal motions are also considered. A non-dimensional system of notation is used, and problems are included at the end of chapters. This book is comprised of 13 chapters and begins with an introduction to aircraft static stability and maneuverability, with emphasis on the theoretical basis of flight dynamics and the technical terms used. The physical background for the estimation of aerodynamic derivatives is discussed. Subsequent chapters focus on the longitudinal and lateral motion of aircraft, including the effect of automatic control; modern developments such as the effects of aeroelasticity, dynamic coupling, and high incidence; and aircraft response to gusts. The final chapter demonstrates how to estimate the aerodynamic derivatives, and hence the dynamic stability characteristics, of a typical fighter aircraft. Throughout the text, the aircraft and its behavior are kept well to the fore. This monograph is intended for undergraduate students of aeronautical engineering and for newcomers to the aircraft industry.

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Présentation de l'éditeur

Aircraft Dynamic Stability and Response deals with the fundamentals of dynamic stability in aircraft. Topics covered include flight dynamics, equations of motion, and lateral and longitudinal aerodynamic derivatives. Basic lateral and longitudinal motions are also considered. A non-dimensional system of notation is used, and problems are included at the end of chapters. This book is comprised of 13 chapters and begins with an introduction to aircraft static stability and maneuverability, with emphasis on the theoretical basis of flight dynamics and the technical terms used. The physical background for the estimation of aerodynamic derivatives is discussed. Subsequent chapters focus on the longitudinal and lateral motion of aircraft, including the effect of automatic control; modern developments such as the effects of aeroelasticity, dynamic coupling, and high incidence; and aircraft response to gusts. The final chapter demonstrates how to estimate the aerodynamic derivatives, and hence the dynamic stability characteristics, of a typical fighter aircraft. Throughout the text, the aircraft and its behavior are kept well to the fore. This monograph is intended for undergraduate students of aeronautical engineering and for newcomers to the aircraft industry.

Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.

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9780080247694: Aircraft Dynamic Stability and Response

Edition présentée

ISBN 10 :  0080247695 ISBN 13 :  9780080247694
Editeur : Pergamon Press, 1980
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Babister, A. W.
Edité par Pergamon, 1980
ISBN 10 : 0080247687 ISBN 13 : 9780080247687
Ancien ou d'occasion Couverture souple

Vendeur : Anybook.com, Lincoln, Royaume-Uni

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Etat : Fair. This is an ex-library book and may have the usual library/used-book markings inside.This book has soft covers. Book contains pencil 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:0080247687. N° de réf. du vendeur 9928059

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A. W. Babister
Edité par Pergamon, 1980
ISBN 10 : 0080247687 ISBN 13 : 9780080247687
Neuf Paperback

Vendeur : Revaluation Books, Exeter, Royaume-Uni

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Paperback. Etat : Brand New. 246 pages. 9.80x6.77x0.98 inches. In Stock. N° de réf. du vendeur zk0080247687

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