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100   $a20111115j198012    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 /$fRobert L. Stallings, Jr., and Milton Lamb
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dDecember 1980.
215   $a1 online resource (45 pages) $cillustrations
225 1 $aNASA technical paper ;$v1789
300   $aTitle from title screen (viewed on Aug. 23, 2016).
300   $a"December 1980."
300   $a"Performing Organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 17-18).
606   $aBoundary layer flow$2nasat
606   $aBoundary layer stability$2nasat
606   $aHeat transfer$2nasat
606   $aReynolds number$2nasat
606   $aWind tunnel tests$2nasat
606   $aAerothermodynamics$2fast
606   $aBoundary layer$2fast
606   $aSupersonic wind tunnels$2fast
615  7$aBoundary layer flow.
615  7$aBoundary layer stability.
615  7$aHeat transfer.
615  7$aReynolds number.
615  7$aWind tunnel tests.
615  7$aAerothermodynamics.
615  7$aBoundary layer.
615  7$aSupersonic wind tunnels.
700   $aStallings$b Robert L.$01396665
702   $aLamb$b Milton
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910707438603321
996   $aWind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3$93513904
997   $aUNINA