01818nam 2200517 450 991070209160332120130115142629.0(CKB)5470000002423208(OCoLC)824429524(EXLCZ)99547000000242320820130115d2012 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierQuantitative global heat transfer in a Mach-6 quiet tunnel /John P. Sullivan [and ten others]Hampton, Va.:National Aeronautics and Space Administration, Langley Research Center,[2012]1 online resource (148 pages) color illustrations[NASA contractor report] ;NASA-CR 2012-217331Title from title screen (viewed Jan. 15, 2013)."February 2012."Includes bibliographical references (pages 126-128).Heat transfernasatHypersonic speednasatTemperature sensitive paintsnasatWind tunnel testsnasatHypersonic wind tunnelsnasatHeat fluxnasatMathematical modelsnasatHeat transfer.Hypersonic speed.Temperature sensitive paints.Wind tunnel tests.Hypersonic wind tunnels.Heat flux.Mathematical models.Sullivan John P.921953Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702091603321Quantitative global heat transfer in a Mach-6 quiet tunnel3530619UNINA