Active spanwise lift control : a distributed parameter approach

"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 authori...

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Bibliographic Details
Main Authors: Dias, Joaquim Neto, (Author), Hubbard, James E., Jr. 1951- (Author)
Format: eBook
Language: English
Published: Reston, Virginia : American Institute of Aeronautics and Astronautics, Inc., [2020]
Series: AIAA education series.
Subjects:
Lift (Aerodynamics)
Gust loads.
Airplanes > Wings.
Trailing edge flaps.
elektronické knihy
electronic books
ISBN: 9781523140930
1523140933
9781624105999
Physical Description: 1 online resource (xvii, 184 pages) : illustrations (some color)

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Table of contents

LEADER 02640cam a2200433 i 4500
001 kn-on1308992371
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 220405t20202020vaua ob 001 0 eng
040 |a HUA  |b eng  |e rda  |c HUA  |d OCLCO  |d OCLCF  |d YDX  |d OCLCO  |d OCLCL 
020 |a 9781523140930  |q (electronic book) 
020 |a 1523140933  |q (electronic book) 
020 |z 9781624105999  |q (print) 
035 |a (OCoLC)1308992371 
100 1 |a Dias, Joaquim Neto,  |e author. 
245 1 0 |a Active spanwise lift control :  |b a distributed parameter approach /  |c Joaquim Neto Dias, James E. Hubbard. 
264 1 |a Reston, Virginia :  |b American Institute of Aeronautics and Astronautics, Inc.,  |c [2020] 
264 4 |c ©2020 
300 |a 1 online resource (xvii, 184 pages) :  |b illustrations (some color) 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a AIAA education series 
504 |a Includes bibliographical references (pages 173-180) and index. 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
520 |a "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"--  |c Provided by publisher. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Lift (Aerodynamics) 
650 0 |a Gust loads. 
650 0 |a Airplanes  |x Wings. 
650 0 |a Trailing edge flaps. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Hubbard, James E.,  |c Jr.  |q (James Edward),  |d 1951-  |e author.  |1 https://id.oclc.org/worldcat/entity/E39PCjF8gKG4vBW3Jmb8gy7yMK 
776 0 8 |i Print version:  |a Dias, Joaquim Neto.  |t Active spanwise lift control.  |d Reston, Virginia : American Institute of Aeronautics and Astronautics, Inc., [2020]  |h xvii, 184 pages : illustrations (some color) ; 24 cm  |w (OCoLC)1193557895 
830 0 |a AIAA education series. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpASLCADP7/active-spanwise-lift?kpromoter=marc  |y Full text 

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