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Les informations fournies dans la section « Synopsis » peuvent faire référence à une autre édition de ce titre.
Bandu N. Pamadi is a senior aerospace engineer at NASA Langley Research Center. He was a German academic exchange fellow at the University of Stuttgart from 1973–1975 and an NRC-NASA Research Associate at NASA Langley from 1981–1983. Before returning to NASA Langley in 1986, he was a professor of aeronautical engineering at the Indian Institute of Technology, Bombay. He holds degrees from Karnatak University, the Indian Institute of Science, Bangalore, and the Indian Institute of Technology, Bombay.
Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.
EUR 17,23 expédition depuis Etats-Unis vers France
Destinations, frais et délaisEUR 17,23 expédition depuis Etats-Unis vers France
Destinations, frais et délaisVendeur : GreatBookPrices, Columbia, MD, Etats-Unis
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Etat : New. Provides a comprehensive and integrated overview of several interrelated disciplines involving airplane performance. The book contains all necessary background material on aerodynamics, dynamics, and control systems, discussing the fundamental principles wi. N° de réf. du vendeur 596449960
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hardcover. Etat : New. Third. Ships same day or next business day! UPS shipping available (Priority Mail for AK/HI/APO/PO Boxes). Used sticker and some writing and/or highlighting. Used books may not include working access code. Used books will not include dust jackets. N° de réf. du vendeur 002026947N
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Hardcover. Etat : new. Hardcover. Performance, Stability, Dynamics and Control of Airplanes provides a comprehensive and integrated overview of several interrelated disciplines involving airplane performance. It contains all necessary background material on aerodynamics, dynamics, and control systems, discussing the fundamental principles with the use of sketches, solved examples, and design exercises. It is an ideal text for upper level undergraduates, graduate students, and professionals. Chapters 1 through 3 present basic principles of aerodynamics, aircraft performance, and static equilibrium and control in steady flight. Chapter 4 deals with aircraft dynamics and decoupled equations for longitudinal and lateral motion, and it introduces the concept of stability derivatives. Chapter 5 discusses design of stability augmentation systems and autopilots. Chapter 6 discusses aircraft response and methods of closed-loop control of aircraft, while Chapters 7 and 8 discuss problems of inertial coupling, aircraft spin, and high angle of attack. The third edition features updates throughout along with a new chapter 9 on stability, control issues, and challenges of unmanned aerial vehicles Provides a comprehensive and integrated overview of several interrelated disciplines involving airplane performance. The book contains all necessary background material on aerodynamics, dynamics, and control systems, discussing the fundamental principles with the use of sketches, solved examples, and design exercises. Shipping may be from multiple locations in the US or from the UK, depending on stock availability. N° de réf. du vendeur 9781624102745
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Etat : good. A good reading copy. May contain markings or be a withdrawn library copy. N° de réf. du vendeur 9781624102745-4
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