02500oam 2200745I 450 991070979300332120180615105023.0(CKB)5470000002472312(OCoLC)761260747(EXLCZ)99547000000247231220111115j198506 ua 0engurun||||a|a||txtrdacontentcrdamediacrrdacarrierLee-side flow over delta wings at supersonic speeds /David S. Miller and Richard M. WoodWashington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Branch,June 1985.1 online resource (iii, 150 pages) illustrationsNASA/TP ;2430"June 1985."Prepared at Langley Research Center.Includes bibliographical references (page 150).Delta wingsnasatFlow characteristicsnasatLeading edgesnasatFlow visualizationnasatPressure measurementnasatAerodynamics, SupersonicAirplanesWings, TriangularVortex-motionLeading edges (Aerodynamics)Aerodynamics, SupersonicfastAirplanesWings, TriangularfastLeading edges (Aerodynamics)fastVortex-motionfastDelta wings.Flow characteristics.Leading edges.Flow visualization.Pressure measurement.Aerodynamics, Supersonic.AirplanesWings, Triangular.Vortex-motion.Leading edges (Aerodynamics)Aerodynamics, Supersonic.AirplanesWings, Triangular.Leading edges (Aerodynamics)Vortex-motion.Miller David S.1414616Wood Richard M.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,Langley Research Center.OCLCEOCLCEOCLCQOCLCFOCLCQOCLCOOCLCQGPOBOOK9910709793003321Lee-side flow over delta wings at supersonic speeds3514463UNINA