Introduction to Aircraft Aeroelasticity and Loads, 2e
Jan R. Wright, University of Manchester;
Jonathan E. Cooper, University of Liverpool
John Wiley & Sons, Inc., 2015
ISBN: 978-1-118-48801-0;
Language: English
Written for undergraduate and graduate students, as well as engineers who are new to the aerospace industry, Introduction to Aircraft Aeroelasticity and Loads introduces the foundations of aeroelasticity and loads for the flexible aircraft. It provides an understanding of the main concepts involved and relates them to aircraft behavior and industrial practice. Topics 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.
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