LEADER 01054cam0-22003851i-450- 001 990006765270403321 005 20131107113258.0 010 $a88-343-6915-7 035 $a000676527 035 $aFED01000676527 035 $a(Aleph)000676527FED01 035 $a000676527 100 $a20010426d1991----km-y0itay50------ba 101 0 $aita 102 $aIT 105 $ay-------001yy 200 1 $a<>scambi commerciali della comunita europea$fPaolo Gramatica 210 $aMilano$cVita e Pensiero$d1991 215 $a527 p.$d24 cm 225 1 $aTrattati e manuali 610 0 $aMec , Geografia Economica 676 $a382.9 676 $a050.031 700 1$aGramatica,$bPaolo$0129343 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990006765270403321 952 $aVII A 419$b19407$fFSPBC 952 $a050.031.GRA.$b1079/B$fDECGE 952 $aISVE F1-F4.81$fDECTS 959 $aFSPBC 959 $aDECGE 959 $aDECTS 996 $aScambi commerciali della Comunità europea$9198246 997 $aUNINA LEADER 00748nam0-22002771i-450- 001 990003480590403321 005 20131024153836.0 035 $a000348059 035 $aFED01000348059 035 $a(Aleph)000348059FED01 035 $a000348059 100 $a20030910d1984----km-y0itay50------ba 101 0 $aita 105 $ay-------001yy 200 1 $aDeveloping South Asia$eA Modernization perspective$fa cura di P.K. Ghosh 210 $aWestport$cs.e.$d1984 702 1$aGhosh P.K. 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990003480590403321 952 $aSE 039.08.03-$b5101$fDECSE 952 $aISVE O01.65$fDECTS 959 $aDECSE 959 $aDECTS 996 $aDeveloping South Asia$9496093 997 $aUNINA LEADER 01505oam 2200445 450 001 9910717012003321 005 20220218115047.0 035 $a(CKB)5470000002528090 035 $a(OCoLC)1291212594 035 $a(OCoLC)995470000002528090 035 $a(EXLCZ)995470000002528090 100 $a20220106j199204 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model /$fAparajit J. Mahajan [and three others] 210 1$aWashington, D.C. :$cNASA,$dApril 1992. 215 $a1 online resource (approximately 14 pages) $cillustrations 225 1 $aNASA/TM ;$v105268 300 $a"April 1992." 320 $aIncludes bibliographical references (pages 6-7). 606 $aProp-fan technology$2nasat 606 $aFlutter$2nasat 606 $aCruise missiles$2nasat 615 7$aProp-fan technology. 615 7$aFlutter. 615 7$aCruise missiles. 700 $aMahajan$b Aparajit J$g(Aparajit Jagannath),$01419987 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 801 2$bGPO 801 2$bOCLCO 801 2$bGPO 906 $aBOOK 912 $a9910717012003321 996 $aAeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model$93536332 997 $aUNINA