LEADER 02440nam 2200505 450 001 9910795900903321 005 20230118184457.0 010 $a1-62410-630-7 010 $a1-5231-4093-3 035 $a(CKB)5590000000638898 035 $a(MiAaPQ)EBC29275813 035 $a(Au-PeEL)EBL29275813 035 $a(EXLCZ)995590000000638898 100 $a20230118d2020 uy 0 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aActive spanwise lift control $ea distributed parameter approach /$fJoaquim Neto Dias, Experimental Flight Test Engineer, Captain, Brazilian Air Force, Flight Test and Research Institute (IPEV), Sa?o Jose? dos Campos, Sa?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 205 $a1st ed. 210 1$aReston, Virginia :$cAmerican Institute of Aeronautics and Astronautics, Inc.,$d[2020] 210 4$dİ2020 215 $a1 online resource (205 pages) 311 $a1-62410-599-8 320 $aIncludes bibliographical references and index. 330 $aActive Spanwise Lift Control 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. 606 $aGust loads 606 $aLift (Aerodynamics) 606 $aTrailing edge flaps 606 $aAirplanes$xWings 615 0$aGust loads. 615 0$aLift (Aerodynamics) 615 0$aTrailing edge flaps. 615 0$aAirplanes$xWings. 676 $a629.13233 700 $aDias$b Joaquim Neto$01506198 702 $aHubbard$b James E.$cJr.$g(James Edward),$f1951- 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910795900903321 996 $aActive spanwise lift control$93736304 997 $aUNINA