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035   $a(OCoLC)760932694
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100   $a20111114j198009    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLow-pressure performance of annular, high-pressure (40-atm), high-temperature, (2480 K) combustion system /$fJerrold D. Wear, Arthur M. Trout, and John M. Smith
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dSeptember 1980.
215   $a1 online resource (ii, 18 pages) $cillustrations
225 1 $aNASA technical paper ;$v1713
300   $aTitle from title screen (viewed on Aug. 16, 2016).
300   $a"September 1980."
300   $a"Performing Organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 5-6).
517   $aLow-pressure performance of annular, high-pressure 
606   $aCombustion efficiency$2nasat
606   $aExhaust gases$2nasat
606   $aFuel injection$2nasat
606   $aFuel-air ratio$2nasat
606   $aInlet temperature$2nasat
615  7$aCombustion efficiency.
615  7$aExhaust gases.
615  7$aFuel injection.
615  7$aFuel-air ratio.
615  7$aInlet temperature.
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$bOCLCQ
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910707472703321
996   $aLow-pressure performance of annular, high-pressure (40-atm), high-temperature, (2480 K) combustion system$93434683
997   $aUNINA