LEADER 01404nam 2200385 450 001 000016087 005 20050718115600.0 010 $a0-8247-6555-9 100 $a20030902d1976----km-y0itay0103----ba 101 0 $aeng 102 $aUS 200 1 $aAnti-invariant submanifolds$fKentaro Yano, Masahiro Kon 210 $aNew York ; Basel$cMarcel Dekker$dc1976 215 $aVII, 183 p.$d26 cm. 225 2 $aLecture notes in pure and applied mathematics$v21 410 0$12001$aLecture notes in pure and applied mathematics 606 $aGeometria differenziale 676 $a516.36$v(21. ed.)$9Geometria differenziale e integrale 691 $a53C40$9Differential geometry. Global differential geometry. Global submanifolds 700 1$aYano,$bKentaro$051358 701 1$aKon,$bMasahiro$051359 801 0$aIT$bUniversità della Basilicata - B.I.A.$gRICA$2unimarc 912 $a000016087 996 $aAnti-invariant submanifolds$982269 997 $aUNIBAS BAS $aMONSCI BAS $aSCIENZE CAT $aEXT002$b01$c20030902$lBAS01$h1222 CAT $c20050601$lBAS01$h1755 CAT $abatch$b01$c20050718$lBAS01$h1052 CAT $c20050718$lBAS01$h1112 CAT $c20050718$lBAS01$h1142 CAT $c20050718$lBAS01$h1156 FMT Z30 -1$lBAS01$LBAS01$mBOOK$1BASA2$APolo Tecnico-Scientifico$2GEN$BCollezione generale$3MAT$663342$5S63342$820030902$f51$FRiservati LEADER 01870nam 2200505 450 001 9910705661603321 005 20170908151141.0 035 $a(CKB)5470000002451780 035 $a(OCoLC)986800984 035 $a(EXLCZ)995470000002451780 100 $a20170511j200210 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aMethodology of blade unsteady pressure measurement in the NASA transonic flutter cascade /$fJ. Lepicovsky [and four others] 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dOctober 2002. 215 $a1 online resource (49 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2002-211894 300 $a"October 2002." 300 $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page. 320 $aIncludes bibliographical references (pages 17-18). 606 $aTransonic flutter$2nasat 606 $aUnsteady aerodynamics$2nasat 606 $aRotary wings$2nasat 606 $aComputerized simulation$2nasat 606 $aWind tunnels$2nasat 606 $aPressure measurement$2nasat 606 $aData integration$2nasat 615 7$aTransonic flutter. 615 7$aUnsteady aerodynamics. 615 7$aRotary wings. 615 7$aComputerized simulation. 615 7$aWind tunnels. 615 7$aPressure measurement. 615 7$aData integration. 700 $aLepicovsky$b Jan$01393046 712 02$aNASA Glenn Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910705661603321 996 $aMethodology of blade unsteady pressure measurement in the NASA transonic flutter cascade$93448666 997 $aUNINA