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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...
| Autores principales: | , |
|---|---|
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Reston, Virginia :
American Institute of Aeronautics and Astronautics, Inc.,
[2020]
|
| Colección: | AIAA education series.
|
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | KNOVEL_on1308992371 | ||
| 003 | OCoLC | ||
| 005 | 20231027140348.0 | ||
| 006 | m o d | ||
| 007 | cr bn||||||||| | ||
| 008 | 220405t20202020vaua ob 001 0 eng | ||
| 040 | |a HUA |b eng |e rda |c HUA |d OCLCO |d OCLCF |d YDX | ||
| 020 | |a 9781523140930 |q (electronic book) | ||
| 020 | |a 1523140933 |q (electronic book) | ||
| 020 | |z 9781624105999 |q (print) | ||
| 029 | 1 | |a AU@ |b 000073247426 | |
| 029 | 1 | |a AU@ |b 000070439085 | |
| 035 | |a (OCoLC)1308992371 | ||
| 082 | 0 | 4 | |a 629.13233 |2 23 |
| 049 | |a UAMI | ||
| 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 Ã2020 | |
| 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. | ||
| 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 ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Lift (Aerodynamics) | |
| 650 | 0 | |a Gust loads. | |
| 650 | 0 | |a Airplanes |x Wings. | |
| 650 | 0 | |a Trailing edge flaps. | |
| 650 | 6 | |a Portance. | |
| 650 | 6 | |a Avions |x Ailes. | |
| 650 | 7 | |a Airplanes |x Wings. |2 fast |0 (OCoLC)fst00803545 | |
| 650 | 7 | |a Gust loads. |2 fast |0 (OCoLC)fst00949518 | |
| 650 | 7 | |a Lift (Aerodynamics) |2 fast |0 (OCoLC)fst00998431 | |
| 650 | 7 | |a Trailing edge flaps. |2 fast |0 (OCoLC)fst01154416 | |
| 700 | 1 | |a Hubbard, James E., |c Jr. |q (James Edward), |d 1951- |e author. | |
| 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://appknovel.uam.elogim.com/kn/resources/kpASLCADP7/toc |z Texto completo |
| 938 | |a YBP Library Services |b YANK |n 17948131 | ||
| 994 | |a 92 |b IZTAP | ||