Product details:
ISBN13: | 9781108420600 |
ISBN10: | 1108420605 |
Binding: | Hardback |
No. of pages: | 566 pages |
Size: | 249x175x34 mm |
Weight: | 1070 g |
Language: | English |
720 |
Category:
Dynamics of Flexible Aircraft
Coupled Flight Mechanics, Aeroelasticity, and Control
Series:
Cambridge Aerospace Series;
52;
Publisher: Cambridge University Press
Date of Publication: 13 July 2023
Normal price:
Publisher's listprice:
GBP 99.99
GBP 99.99
Your price:
38 636 (36 796 HUF + 5% VAT )
discount is: 20% (approx 9 659 HUF off)
Discount is valid until: 30 June 2024
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Availability:
Estimated delivery time: In stock at the publisher, but not at Prospero's office. Delivery time approx. 3-5 weeks.
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Short description:
Explore the interface between aeroelasticity, flight dynamics and control in this fresh approach, featuring numerous hands-on examples.
Long description:
Explore the connections among aeroelasticity, flight dynamics, and control with an up-to-date multidisciplinary approach. New insights into the interaction between these fields, which is a distinctive feature of many modern aircraft designed for very high aerodynamic efficiency, are fully illustrated in this one-of-a-kind book. Presenting basic concepts in a systematic and rigorous, yet accessible way, this book builds up to state-of-the-art models through an intuitive step-by-step approach. Both linear and nonlinear attributes are covered and, by revisiting classical solutions using modern analysis methods, this book provides a unique perspective to bridge the gap between disciplines. Numerous original numerical examples, including online source codes, help to build intuition through hands-on activities. This book will empower the reader to design better and more environmentally friendly aircraft, and is an ideal resource for graduate students, researchers, and aerospace engineers.
Table of Contents:
1. Introduction; 2. The non-stationary atmosphere; 3. Dynamics of elastically-supported rigid airfoils; 4. Dynamics of rigid aircraft in a non-stationary atmosphere; 5. Dynamics of flexible aircraft with quasi-steady deformations; 6. Dynamics of flexible aircraft with small-amplitude vibrations; 7. Time-domain unsteady aerodynamics for low-speed flight 8. Geometrically-nonlinear composite beams; 9. Dynamics of very flexible aircraft; 10. Feedback control; 11. Experimental testing; Appendices.