"This book presents a novel approach to tackle the gust alleviation problem. Traditional approaches typically attempt to suppress the structural response at discrete points of the wing using only the conventional control surfaces (aileron, elevator, rudder), resulting in limited control authority, high-bandwidth actuator requirements, and necessity of gust field measurements ahead of the aircraft. In this book, the authors directly address the spanwise behavior of aerodynamic loads, as this is what should be primarily controlled"--
Active spanwise lift control : a distributed parameter approach
2020
xvii, 184 Seiten
Illustrationen
Includes bibliographical references and index
Buch
Englisch
BKL: | 50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik | |
DDC: | 629.132/33 |
Lift Prediction of Spanwise Cambered Delta Wings
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|Augmentation of Vortex Lift by Spanwise Blowing
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|Augmentation of vortex lift by spanwise blowing
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