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035   $a(OCoLC)761335595
035   $a(EXLCZ)995470000002465153
100   $a20111115j198103    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPerformance of semi-transpiration-cooled liner in high-temperature-rise combustor /$fJerrold D. Wear, Arthur M. Trout and John M. Smith
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dMarch 1981.
215   $a1 online resource (17 pages) $cillustrations
225 1 $aNASA technical paper ;$v1806
300   $aTitle from title screen (viewed on Aug. 25, 2016).
300   $a"March 1981."
300   $a"Performing Organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 17).
606   $aCombustion efficiency$2nasat
606   $aFuel injection$2nasat
606   $aFuel-air ratio$2nasat
606   $aStoichiometry$2nasat
606   $aThermodynamic efficiency$2nasat
615  7$aCombustion efficiency.
615  7$aFuel injection.
615  7$aFuel-air ratio.
615  7$aStoichiometry.
615  7$aThermodynamic efficiency.
700   $aWear$b Jerrold D.$01386080
702   $aTrout$b Arthur M.
702   $aSmith$b John M$g(John Milton),$f1922-
712 02$aLewis Research Center.
712 02$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   $a9910707437703321
996   $aPerformance of semi-transpiration-cooled liner in high-temperature-rise combustor$93465241
997   $aUNINA