02399oam 2200601 450 991070268300332120140922114318.0(CKB)5470000002429356(OCoLC)761863635(EXLCZ)99547000000242935620111122j197912 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 /Jim A. Penland, James B. Hallissy, and James L. DillonWashington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Branch,December 1979.1 online resource (144 pages) illustrationsNASA technical paper ;1552Title from title screen (viewed Sept. 22, 2014)."December 1979.""Performing organization, NASA Langley Research Center"--Technical report documentation page.Includes bibliographical references (pages 20-22).AerodynamicsAerodynamic characteristicsnasatComputational fluid dynamicsnasatDelta wingsnasatHypersonic aircraftnasatWind tunnel testsnasatAerodynamicsfastAerodynamics.Aerodynamic characteristics.Computational fluid dynamics.Delta wings.Hypersonic aircraft.Wind tunnel tests.Aerodynamics.Penland Jim A.1416903Hallissy James B.Dillon James L.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,Langley Research Center,OCLCEOCLCEOCLCQOCLCFOCLCQGPOBOOK9910702683003321Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.03525942UNINA