01946oam 2200505I 450 991070700950332120160405151742.0(CKB)5470000002461397(OCoLC)703663798(EXLCZ)99547000000246139720110224j199609 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierEvaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers /Patrick C. Stoliker and John T. BosworthEdwards, California :National Aeronautics and Space Administration, Dryden Flight Research Center,September 1996.1 online resource (32 pages) illustrationsNASA technical memorandum ;104322Title from title screen (viewed April 5, 2016)."September 1996.""Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.Includes bibliographical references (pages 31-32).Aircraft maneuversnasatAngle of attacknasatFlight controlnasatPilot induced oscillationnasatX-31 aircraftnasatAircraft maneuvers.Angle of attack.Flight control.Pilot induced oscillation.X-31 aircraft.Stoliker P. C.1389353Bosworth John T.NASA Dryden Flight Research Center,United States.National Aeronautics and Space Administration,SSNSSNGPOBOOK9910707009503321Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers3440793UNINA