LEADER 01818nam  2200517   450 
001 9910702091603321
005 20130115142629.0
035   $a(CKB)5470000002423208
035   $a(OCoLC)824429524
035   $a(EXLCZ)995470000002423208
100   $a20130115d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aQuantitative global heat transfer in a Mach-6 quiet tunnel /$fJohn P. Sullivan [and ten others]
210  1$aHampton, Va.:$cNational Aeronautics and Space Administration, Langley Research Center,$d[2012]
215   $a1 online resource (148 pages) $ccolor illustrations
225 1 $a[NASA contractor report] ;$vNASA-CR 2012-217331
300   $aTitle from title screen (viewed Jan. 15, 2013).
300   $a"February 2012."
320   $aIncludes bibliographical references (pages 126-128).
606   $aHeat transfer$2nasat
606   $aHypersonic speed$2nasat
606   $aTemperature sensitive paints$2nasat
606   $aWind tunnel tests$2nasat
606   $aHypersonic wind tunnels$2nasat
606   $aHeat flux$2nasat
606   $aMathematical models$2nasat
615  7$aHeat transfer.
615  7$aHypersonic speed.
615  7$aTemperature sensitive paints.
615  7$aWind tunnel tests.
615  7$aHypersonic wind tunnels.
615  7$aHeat flux.
615  7$aMathematical models.
700   $aSullivan$b John P.$0921953
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702091603321
996   $aQuantitative global heat transfer in a Mach-6 quiet tunnel$93530619
997   $aUNINA