Rafael Palacios, Carlos E. S. Cesnik

Dynamics of Flexible Aircraft (eBook, PDF)

Coupled Flight Mechanics, Aeroelasticity, and Control

• Format: PDF

Produktbeschreibung

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.

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Produktdetails

• Verlag: Cambridge University Press
• Erscheinungstermin: 13. Juli 2023
• Englisch
• ISBN-13: 9781108359573
• Artikelnr.: 70912920

Autorenporträt

Rafael Palacios is Professor of Computational Aeroelasticity and Director of the Brahmal Vasudevan Institute for Sustainable Aviation at Imperial College, London. He is a fellow of the Royal Aeronautical Society and an associate fellow of the American Institute of Aeronautics and Astronautics.

Inhaltsangabe

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.