01745nam 2200469 a 450 991069704170332120230902162039.0(CKB)5470000002384486(OCoLC)695595245(EXLCZ)99547000000238448620110107d2010 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierEstimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods[electronic resource] /Gary E. EricksonHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2010]1 online resource (v, 36 pages) illustrationsNASA/TM- ;2010-216196Title from title screen (viewed on Jan. 7, 2011)."February 2010."Includes bibliographical references (pages 23-24).NASA technical memorandum ;216196.Aerodynamic characteristicsnasatControl surfacesnasatLaunch vehiclesnasatShock wave interactionnasatSupersonic speednasatAerodynamic characteristics.Control surfaces.Launch vehicles.Shock wave interaction.Supersonic speed.Erickson Gary E1403144Langley Research Center.GPOGPOBOOK9910697041703321Estimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods3519399UNINA