02101nam 2200589I 450 991070807070332120170315160924.0(CKB)5470000002469870(OCoLC)976012018(EXLCZ)99547000000246987020170315j199704 ba 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierVertical tail buffeting alleviation using piezoelectric actuatorssome results of the Actively Controlled Response of Buffet-Affected Tails (ACROBAT) program /Robert W. MosesHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,April 1997.1 online resource (18 pages) illustrationsNASA technical memorandum ;110336"April 1997.""Performing organization: NASA Langley Research Center" Report documentation page.Includes bibliographical references (pages 17-18).Vertical tail buffeting alleviation using piezoelectric actuators PiezoelectricitynasatBuffetingnasatActive controlnasatTail assembliesnasatSupersonic aircraftnasatVorticesnasatAngle of attacknasatAeroelasticitynasatLeading edgesnasatRoot-mean-square errorsnasatPiezoelectricity.Buffeting.Active control.Tail assemblies.Supersonic aircraft.Vortices.Angle of attack.Aeroelasticity.Leading edges.Root-mean-square errors.Moses Robert W.1387211Langley Research Center,GPOGPOBOOK9910708070703321Vertical tail buffeting alleviation using piezoelectric actuators3483396UNINA