Dynamics of Flexible Aircraft
Coupled Flight Mechanics, Aeroelasticity, and Control
Series: Cambridge Aerospace Series; 52;
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47 770 Ft (45 495 Ft + 5% VAT)
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47 770 Ft
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Estimated delivery time: Expected time of arrival: end of January 2026.
Not in stock at Prospero.
Why don't you give exact delivery time?
Delivery time is estimated on our previous experiences. We give estimations only, because we order from outside Hungary, and the delivery time mainly depends on how quickly the publisher supplies the book. Faster or slower deliveries both happen, but we do our best to supply as quickly as possible.
Product details:
- Publisher Cambridge University Press
- Date of Publication 13 July 2023
- ISBN 9781108420600
- Binding Hardback
- No. of pages526 pages
- Size 249x175x34 mm
- Weight 1070 g
- Language English 530
Categories
Short description:
Explore the interface between aeroelasticity, flight dynamics and control in this fresh approach, featuring numerous hands-on examples.
MoreLong 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.
MoreTable 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.
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