LEADER 00963nam1-22003011i-450- 001 990004025370403321 005 20130507132617.0 035 $a000402537 035 $aFED01000402537 035 $a(Aleph)000402537FED01 035 $a000402537 100 $a19990604d1984----km-y0itay50------ba 101 0 $afre 105 $ay-------001yy 200 1 $a<>colleges français XVI-XVIII siècles$fMarie-Madeleine Compère, Dominique Julia 210 $aParis$cINRP$cCNRS$d1984 215 $av.$d25 cm 463 \1$1001990005800260403321$12001 $aFrance du Midi 700 1$aCompère,$bMarie-Madeleine$f<1946-2007>$0384418 701 1$aJulia,$bDominique$f<1940- >$0143726 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990004025370403321 952 $a016.371 COMP 1 bis$bD.D.S.1094$fFLFBC 952 $a016.371 COMP 1$bD.D.S. 670$fFLFBC 959 $aFLFBC 996 $aColleges français XVI-XVIII siècles$9470319 997 $aUNINA LEADER 01615nam 2200469I 450 001 9910705713903321 005 20170707085648.0 035 $a(CKB)5470000002453272 035 $a(OCoLC)992989283 035 $a(EXLCZ)995470000002453272 100 $a20170707j201705 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aInlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility /$fRichard F. Bozak 210 1$aCleveland, Ohio:$cNational Aeronautics and Space Administration, Glenn Research Center,$dMay 2017. 215 $a1 online resource (6 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2017-219489 300 $a"May 2017." 320 $aIncludes bibliographical references (page 2). 606 $aAcoustic properties$2nasat 606 $aAerodynamic characteristics$2nasat 606 $aBypass ratio$2nasat 606 $aNoise reduction$2nasat 606 $aRotors$2nasat 606 $aTurbofan engines$2nasat 615 7$aAcoustic properties. 615 7$aAerodynamic characteristics. 615 7$aBypass ratio. 615 7$aNoise reduction. 615 7$aRotors. 615 7$aTurbofan engines. 700 $aBozak$b Richard F.$01405259 712 02$aNASA Glenn Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910705713903321 996 $aInlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility$93494649 997 $aUNINA