Dynamics of Flexible Aircraft: Coupled Flight Mechanics, Aeroelasticity, and Control
 
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
 
Publisher: Cambridge University Press
Date of Publication:
 
Normal price:

Publisher's listprice:
GBP 99.99
Estimated price in HUF:
48 295 HUF (45 995 HUF + 5% VAT)
Why estimated?
 
Your price:

38 636 (36 796 HUF + 5% VAT )
discount is: 20% (approx 9 659 HUF off)
Discount is valid until: 30 June 2024
The discount is only available for 'Alert of Favourite Topics' newsletter recipients.
Click here to subscribe.
 
Availability:

Estimated delivery time: In stock at the publisher, but not at Prospero's office. Delivery time approx. 3-5 weeks.
Not in stock at Prospero.
Can't you provide more accurate information?
 
  Piece(s)

 
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.