LEADER 01185nam--2200397---450- 001 990002931990203316 005 20080221084716.0 010 $a88-7770-360-1 035 $a000293199 035 $aUSA01000293199 035 $a(ALEPH)000293199USA01 035 $a000293199 100 $a20070524d1993----km-y0itay50------ba 101 1 $aita$crus 102 $aIT 105 $ay|||z|||001yy 200 1 $aNote non casuali$fBoris Lunin$g[prefazione di Jurij Naghibin$gtraduzione di Nina Cechovskaja] 210 $aMilano$cSpirali/Vel$d1993 215 $a153 p.$d22 cm 225 2 $aRomanzi$v71 410 0$12001$aRomanzi 454 1$12001$aNeslucajneye zamety$931649 676 $a891.7842 700 1$aLUNIN,$bBoris$0597199 702 1$aNAGHIBIN,$bJurij Markovic 702 1$aCECHOVSKAJA,$bNina 801 0$aIT$bsalbc$gISBD 912 $a990002931990203316 951 $aVIII.1.A. 860$b198571 L.M.$cVIII.1.$d00159181 959 $aBK 969 $aUMA 979 $aANNAMARIA$b90$c20070524$lUSA01$h1318 979 $aANNAMARIA$b90$c20070528$lUSA01$h1218 979 $aANNAMARIA$b90$c20080221$lUSA01$h0847 996 $aNeslucajneye zamety$931649 997 $aUNISA LEADER 02124oam 2200649I 450 001 9910706169303321 005 20170825125338.0 035 $a(CKB)5470000002454732 035 $a(OCoLC)858255342 035 $a(EXLCZ)995470000002454732 100 $a20130912j199905 ua 0 101 0 $aeng 135 $aurbn||||a|a|| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAeroacoustic data for a high Reynolds number axisymmetric subsonic jet /$fMichael K. Ponton, Lawrence S. Ukeiley, Sang W. Lee 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMay 1999. 215 $a1 online resource (84 pages) $cillustrations 225 1 $aNASA/TM ;$v1999-209336 300 $a"May 1999." 300 $a"Performing organization: NASA Langley Research Center"--Report documentation page. 320 $aIncludes bibliographical references (page 5). 606 $aAeroacoustics$2nasat 606 $aConvergent nozzles$2nasat 606 $aJet flow$2nasat 606 $aSubsonic flow$2nasat 606 $aHigh Reynolds number$2nasat 606 $aPressure oscillations$2nasat 606 $aFlow characteristics$2nasat 606 $aEngine noise$2nasat 606 $aExhaust nozzles$2nasat 606 $aExhaust gases$2nasat 615 7$aAeroacoustics. 615 7$aConvergent nozzles. 615 7$aJet flow. 615 7$aSubsonic flow. 615 7$aHigh Reynolds number. 615 7$aPressure oscillations. 615 7$aFlow characteristics. 615 7$aEngine noise. 615 7$aExhaust nozzles. 615 7$aExhaust gases. 700 $aPonton$b Michael K.$01416815 702 $aUkeiley$b Lawrence S. 702 $aLee$b Sang W. 712 02$aLangley Research Center, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCO 801 2$bOCLCF 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910706169303321 996 $aAeroacoustic data for a high Reynolds number axisymmetric subsonic jet$93523467 997 $aUNINA