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[null,"1.","Record Nr.",null,"UNINA9910806984003321"]
[null,null,"Autore",null,"Dias Joaquim Neto"]
[null,null,"Titolo",null,"Active 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 Park"]
[null,null,"Pubbl/distr/stampa",null,"Reston, Virginia : , : American Institute of Aeronautics and Astronautics, Inc., , [2020]"]
[{"$nulls":4},"©2020"]
[null,null,"ISBN",null,"1-62410-630-7"]
[{"$nulls":4},"1-5231-4093-3"]
[null,null,"Edizione",null,"[1st ed.]"]
[null,null,"Descrizione fisica",null,"1 online resource (205 pages)"]
[null,null,"Disciplina",null,"629.13233"]
[null,null,"Soggetti",null,"Gust loads"]
[{"$nulls":4},"Lift (Aerodynamics)"]
[{"$nulls":4},"Trailing edge flaps"]
[{"$nulls":4},"Airplanes - Wings"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Nota di bibliografia","Includes bibliographical references and index."]
[null,null,null,"Sommario/riassunto","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."]