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100   $a20111115j196811    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aReal-helium hypersonic flow parameters for pressures to 3600 atmospheres and temperatures to 15 000° K /$fby Charles G. Miller III and Sue E. Wilder
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dNovember 1968.
215   $a1 online resource (41 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4869
300   $a"November 1968."
320   $aIncludes bibliographical references (page 23).
606   $aWind tunnels$xTest gases
606   $aVirial coefficients
606   $aHelium$xTesting
606   $aWind tunnels$xFlow visualization
606   $aNewton-Raphson method
606   $aGases at high temperatures$xTesting
606   $aNewton-Raphson method$2fast
606   $aVirial coefficients$2fast
606   $aWind tunnels$xFlow visualization$2fast
606   $aWind tunnels$xTest gases$2fast
615  0$aWind tunnels$xTest gases.
615  0$aVirial coefficients.
615  0$aHelium$xTesting.
615  0$aWind tunnels$xFlow visualization.
615  0$aNewton-Raphson method.
615  0$aGases at high temperatures$xTesting.
615  7$aNewton-Raphson method.
615  7$aVirial coefficients.
615  7$aWind tunnels$xFlow visualization.
615  7$aWind tunnels$xTest gases.
700   $aMiller$b Charles G$g(Charles George),$f1940-$01400398
702   $aWilder$b Sue E.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910714079703321
996   $aReal-helium hypersonic flow parameters for pressures to 3600 atmospheres and temperatures to 15 000° K$93519900
997   $aUNINA