02067nam 2200589I 450 991070234540332120130208163229.0(CKB)5470000002426705(OCoLC)827016717(EXLCZ)99547000000242670520130208d2012 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierFlight test results on the stability and control of the F-15 Quiet Spike aircraft /Cheng M. Moua [and three others]Edwards, CA :National Aeronautics and, Space Administration, Dryden Flight Research Center,[2012]1 online resource (41 pages) color illustrations[NASA technical memorandum] ;NASA/TM 2012-215978Title from title screen (viewed Feb. 8, 2013)."February 2012."Includes bibliographical references (page 15-16).F-15 aircraftnasatFlight testsnasatAircraft controlnasatAircraft stabilitynasatSupersonic flightnasatSonic boomsnasatFuselagesnasatNoses (forebodies)nasatComputational fluid dynamicsnasatFlight controlnasatF-15 aircraft.Flight tests.Aircraft control.Aircraft stability.Supersonic flight.Sonic booms.Fuselages.Noses (forebodies)Computational fluid dynamics.Flight control.Moua Cheng M.1407032Hugh L. Dryden Flight Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702345403321Flight test results on the stability and control of the F-15 Quiet Spike aircraft3487373UNINA