LEADER 00747nam0-22002891i-450- 001 990003320580403321 005 20001010 035 $a000332058 035 $aFED01000332058 035 $a(Aleph)000332058FED01 035 $a000332058 100 $a20001010d--------km-y0itay50------ba 101 0 $aita 105 $ay-------001yy 200 1 $aCONRAD THE NOVELIST 210 $aCambridge$cHarvard University Press$d1965 610 0 $aLetteratura ( Critica ) 676 $a809 700 1$aGuerard,$bAlbert J.$0131820 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990003320580403321 952 $a809 GUE$bLINGUE 47$fDECLI 959 $aDECLI 996 $aConrad the novelist$9181569 997 $aUNINA DB $aING01 LEADER 02220oam 2200577 450 001 9910707472703321 005 20160816133122.0 035 $a(CKB)5470000002464799 035 $a(OCoLC)760932694 035 $a(EXLCZ)995470000002464799 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