MATLAB and Simulink Based Books

Introduction to Aircraft Aeroelasticity and Loads

Introduction to Aircraft Aeroelasticity and Loads

Written for undergraduate and graduate students, as well as engineers who are new to the aerospace industry, this book introduces the foundations of aeroelasticity and loads for the flexible aircraft, providing an understanding of the main concepts involved and relating them to aircraft behavior and industrial practice. Topics covered include fundamentals of structural dynamics, aerodynamics, static and dynamic aeroelasticity, response and load calculations, and testing techniques.

MATLAB and Simulink are used throughout the book to solve many real-world application examples. In addition, a supplemental set of MATLAB M-files and Simulink models is available for download.

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About This Book

Jan R. Wright, University of Manchester
Jonathan E. Cooper, University of Liverpool

John Wiley & Sons, Inc., 2007

ISBN: 978-0470-85840-0
Language: English