02440nam 2200505 450 991079590090332120230118184457.01-62410-630-71-5231-4093-3(CKB)5590000000638898(MiAaPQ)EBC29275813(Au-PeEL)EBL29275813(EXLCZ)99559000000063889820230118d2020 uy 0engurcnu||||||||txtrdacontentcrdamediacrrdacarrierActive spanwise lift control a distributed parameter approach /Joaquim Neto Dias, Experimental Flight Test Engineer, Captain, Brazilian Air Force, Flight Test and Research Institute (IPEV), São José dos Campos, São 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 Park1st ed.Reston, Virginia :American Institute of Aeronautics and Astronautics, Inc.,[2020]©20201 online resource (205 pages)1-62410-599-8 Includes bibliographical references and index.Active 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.Gust loadsLift (Aerodynamics)Trailing edge flapsAirplanesWingsGust loads.Lift (Aerodynamics)Trailing edge flaps.AirplanesWings.629.13233Dias Joaquim Neto1506198Hubbard James E.Jr.(James Edward),1951-MiAaPQMiAaPQMiAaPQBOOK9910795900903321Active spanwise lift control3736304UNINA