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100   $a20111115j198009    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCalculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue /$fH. Harris Hamilton II
210   $aWashington, D.C. $cNational Aeronautics and Space Administration, Scientific and Technical Information Branch$dSeptember1980
215   $a1 online resource (75 pages) $cillustrations
225 1 $aNASA technical paper ;$v1698
300   $aTitle from title screen (viewed on Aug. 10, 2016).
300   $a"September 1980."
300   $a"Performing Organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 40-42).
606   $aAxisymmetric flow$2nasat
606   $aInviscid flow$2nasat
606   $aLaminar heat transfer$2nasat
606   $aStreamlined bodies$2nasat
606   $aThree dimensional boundary layer$2nasat
606   $aBoundary layer$2fast
606   $aLaminar flow$2fast
615  7$aAxisymmetric flow.
615  7$aInviscid flow.
615  7$aLaminar heat transfer.
615  7$aStreamlined bodies.
615  7$aThree dimensional boundary layer.
615  7$aBoundary layer.
615  7$aLaminar flow.
700   $aHamilton$b H. Harris$01405571
712 02$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$bOCLCF
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707488403321
996   $aCalculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue$93536257
997   $aUNINA