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100   $a20120408j196812    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aHeat-transfer coefficients for hydrogen flowing through parallel hexagonal passages at surface temperatures to 2275 K /$fby Jack G. Slaby and William F. Mattson
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1968.
215   $a1 online resource (ii, 22 pages) $cillustrations
225 1 $aNASA/TN ;$vD-4959
300   $a"December 1968."
320   $aIncludes bibliographical references (page 22).
606   $aCoefficients$2nasat
606   $aSurface temperature$2nasat
606   $aGas flow$2nasat
606   $aHoneycomb structures$xThermodynamics
606   $aNuclear fuel elements$xDesign and construction
606   $aNusselt number
606   $aGas flow$2fast
606   $aHeat$xTransmission$2fast
606   $aHoneycomb structures$xThermodynamics$2fast
606   $aHydrogen$xThermal properties$2fast
606   $aNuclear fuel elements$xDesign and construction$2fast
606   $aNusselt number$2fast
615  7$aCoefficients.
615  7$aSurface temperature.
615  7$aGas flow.
615  0$aHoneycomb structures$xThermodynamics.
615  0$aNuclear fuel elements$xDesign and construction.
615  0$aNusselt number.
615  7$aGas flow.
615  7$aHeat$xTransmission.
615  7$aHoneycomb structures$xThermodynamics.
615  7$aHydrogen$xThermal properties.
615  7$aNuclear fuel elements$xDesign and construction.
615  7$aNusselt number.
700   $aSlaby$b Jack G.$01400713
702   $aMattson$b William F.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bAD#
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716081503321
996   $aHeat-transfer coefficients for hydrogen flowing through parallel hexagonal passages at surface temperatures to 2275 K$93548218
997   $aUNINA