01946oam 2200517I 450 991070700890332120160405155643.0(CKB)5470000002461403(OCoLC)703661524(EXLCZ)99547000000246140320110224j199706 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierF/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack /Andrew J. Yuhas [and three others]Edwards, California.:National Aeronautics and Space Administration, Dryden Flight Research Center,June 1997.1 online resource (18 pages) illustrationsNASA technical memorandum ;104327Title from title screen (viewed April 5, 2016)."June 1997.""Under NASA Dryden Flight Research Center contract NAS 3-26617.""Performing organization: Analytical Services & Materials, Inc., Edwards, California [and] General Electric Aircraft Engines, Cincinnati, Ohio"--Report documentation page.Aircraft maneuversnasatAngle of attacknasatDistortionnasatF-18 aircraftnasatInlet flownasatAircraft maneuvers.Angle of attack.Distortion.F-18 aircraft.Inlet flow.Yuhas Andrew J.1421462Analytical Services & Materials, Inc.General Electric Company.Aircraft Engine Business Group.NASA Dryden Flight Research Center,United States.National Aeronautics and Space Administration,SSNSSNGPOBOOK9910707008903321F3542805UNINA