01837nam 2200469 450 991070998130332120180822151746.0(CKB)5470000002474451(OCoLC)1049175261(EXLCZ)99547000000247445120180822j198507 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierExperimental and theoretical study of the 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, 1 unnumbered page) illustrationsNASA/TP ;2433"July 1985."Includes bibliographical references (page 119).Delta wingsnasatSupersonic airfoilsnasatMach numbernasatSweptback wingsnasatSupersonic flownasatDelta wings.Supersonic airfoils.Mach number.Sweptback wings.Supersonic flow.Wood Richard M.144306Covell Peter F.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,Langley Research Center.GPOGPOBOOK9910709981303321Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.163473802UNINA