01991oam 2200529 450 991070979440332120180615095037.0(CKB)5470000002472298(OCoLC)761378019(EXLCZ)99547000000247229820111115j198507 ua 0engurun||||a|a||txtrdacontentcrdamediacrrdacarrierExperimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16 /Richard M. Wood and Peter F. CovellWashington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Branch,July 1985.1 online resource (119 pages) illustrationsNASA/TP ;2433Includes bibliographical references (page 119).Supersonic airfoilsnasatDelta wingsnasatSupersonic flownasatAerodynamic dragnasatMach numbernasatAirplanesWings, TriangularAerodynamicsSupersonic airfoils.Delta wings.Supersonic flow.Aerodynamic drag.Mach number.AirplanesWings, TriangularAerodynamics.Wood Richard M.144306Covell Peter F.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,Langley Research Center.OCLCEOCLCEOCLCQOCLCOOCLCQGPOBOOK9910709794403321Experimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.163504013UNINA