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- 000 02400cam a2200409 i 4500
- 008 200811s2020 vaua b 001 0 eng
- 020 __ |a 9781624105999 |q hardcover
- 020 __ |a 1624105998 |q hardcover
- 035 __ |a (OCoLC)1193557895 |z (OCoLC)1160078117 |z (OCoLC)1160180409
- 040 __ |a DLC |b eng |e rda |c DLC |d OCLCO |d OCLCF |d YDX |d XII |d OCLCO |d YDX
- 050 00 |a TL574.L5 |b D53 2020
- 082 00 |a 629.132/33 |2 23
- 100 1_ |a Dias, Joaquim Neto, |e author.
- 245 10 |a Active spanwise lift control : |b a distributed parameter approach / |c Joaquim Neto Dias, Experimental Flight Test Engineer, Captain, Brazilian Air Force, Flight Test and Research Institute (IPEV), S茫o Jos茅 dos Campos, S茫o Paulo, Brazil, James E. Hubbard, Jr., TEES Eminent Professor, Hagler Institute Fellow, Department of Mechanical Engineering, Texas A&M University, College Station, Texas, USA, Glenn L. Martin Professor Emeritus, University of Maryland, College Park.
- 260 __ |a Reston, Virginia : |b American Institute of Aeronautics and Astronautics, Inc., |c [2020]
- 300 __ |a xvii, 184 pages : |b illustrations (some color) ; |c 24 cm.
- 336 __ |a text |b txt |2 rdacontent
- 337 __ |a unmediated |b n |2 rdamedia
- 338 __ |a volume |b nc |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.
- 650 _0 |a Lift (Aerodynamics)
- 650 _0 |a Airplanes |x Wings.
- 650 _0 |a Trailing edge flaps.
- 650 _7 |a Airplanes |x Wings |2 fast
- 650 _7 |a Gust loads |2 fast
- 650 _7 |a Lift (Aerodynamics) |2 fast
- 650 _7 |a Trailing edge flaps |2 fast
- 700 1_ |a Hubbard, James E., |c Jr. |q (James Edward), |d 1951- |e author.