02167oam 2200589 450 991070748840332120160810142253.0(CKB)5470000002464640(OCoLC)761358552(EXLCZ)99547000000246464020111115j198009 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierCalculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue /H. Harris Hamilton IIWashington, D.C. National Aeronautics and Space Administration, Scientific and Technical Information BranchSeptember19801 online resource (75 pages) illustrationsNASA technical paper ;1698Title from title screen (viewed on Aug. 10, 2016)."September 1980.""Performing Organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 40-42).Axisymmetric flownasatInviscid flownasatLaminar heat transfernasatStreamlined bodiesnasatThree dimensional boundary layernasatBoundary layerfastLaminar flowfastAxisymmetric flow.Inviscid flow.Laminar heat transfer.Streamlined bodies.Three dimensional boundary layer.Boundary layer.Laminar flow.Hamilton H. Harris1405571Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCFOCLCOOCLCQGPOBOOK9910707488403321Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue3536257UNINA