LEADER 01062nam2-2200373---450- 001 990002080350203316 005 20090318105633.0 035 $a000208035 035 $aUSA01000208035 035 $a(ALEPH)000208035USA01 035 $a000208035 100 $a20041014d1968----km-y0itay0103----ba 101 0 $aita 102 $aIT 105 $a||||||||001yy 200 1 $a<<2.>>: Analisi matematica$fFederico Cafiero, Antonio Zitarosa 210 $aNapoli$cLiguori$d1968 215 $a316 p.$d24 cm 410 0$12001 454 1$12001 461 1$1001000208027$12001$aLezioni di matematica generale 606 0 $aAnalisi matematica 676 $a510 700 1$aCAFIERO,$bFederico$0349 701 1$aZITAROSA,$bAntonio$0343247 801 0$aIT$bsalbc$gISBD 912 $a990002080350203316 951 $a510 CAF 1/2 (IS I 36/II)$b9224 E.C.$cIS I$d00202453 959 $aBK 969 $aECO 979 $aSIAV4$b10$c20041014$lUSA01$h0944 979 $aRSIAV2$b90$c20090318$lUSA01$h1056 996 $aAnalisi matematica$91042104 997 $aUNISA LEADER 01792nam 2200469 450 001 9910703769103321 005 20150603125209.0 035 $a(CKB)5470000002434028 035 $a(OCoLC)910630220 035 $a(EXLCZ)995470000002434028 100 $a20150603j201412 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAssessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods /$fGregory P. Herrick 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dDecember 2014. 215 $a1 online resource (17 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2014-218447 300 $aTitle from title screen (viewed on June 3, 2015). 300 $a"December 2014." 300 $a"Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014." 320 $aIncludes bibliographical references (pages 15-17). 606 $aTurbomachinery$2nasat 606 $aFlutter analysis$2nasat 606 $aInlet flow$2nasat 606 $aComputational fluid dynamics$2nasat 606 $aAeroelasticity$2nasat 615 7$aTurbomachinery. 615 7$aFlutter analysis. 615 7$aInlet flow. 615 7$aComputational fluid dynamics. 615 7$aAeroelasticity. 700 $aHerrick$b Gregory Paul$f1972-$01387242 712 02$aNASA Glenn Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910703769103321 996 $aAssessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods$93457802 997 $aUNINA