LEADER 00885nam0-2200277 --450 001 9910509608103321 005 20211207130647.0 010 $a978-88-6242-490-5$bLetteraVentidue 100 $a20211207d2021----kmuy0itay5050----ba 101 $aita$cita 102 $aIT 105 $aa-------001yy 200 1 $a<>emozione puramente visuale$efilm scientifici tra sperimentazione e avanguardia$fMaria Ida Bernabei 210 $aSiracusa$cLetteraVentidue$aVenezia$cIUAV$d2021 215 $a272 p.$cill.$d21 cm 225 1 $aSaggi IUAV$v7$aUniversità IUAV di Venezia 610 0 $aCinema scientifico 676 $a791.4353$v22 700 1$aBernabei,$bMaria Ida$0845148 801 0$aIT$bUNINA$gREICAT$2UNIMARC 901 $aBK 912 $a9910509608103321 952 $aART.VI B$b1211/2021$fFARBC 959 $aFARBC 996 $aEmozione puramente visuale$92541588 997 $aUNINA LEADER 02022nam 2200565 a 450 001 9910701851203321 005 20120618083754.0 035 $a(CKB)5470000002421596 035 $a(OCoLC)795702203 035 $a(EXLCZ)995470000002421596 100 $a20120618d2011 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aBasis function approximation of transonic aerodynamic influence coefficient matrix$b[electronic resource] /$fWesley W. Li and Chan-gi Pak 210 1$aEdwards, CA :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$d[2011] 215 $a1 online resource (17 pages) $cillustrations 225 1 $aNASA/TM ;$v2011-216423 300 $aTitle from title screen (viewed on June 18, 2012). 300 $a"March 2011." 320 $aIncludes bibliographical references (page 17). 606 $aMatrices (mathematics)$2nasat 606 $aTransonic flow$2nasat 606 $aAerodynamic coefficients$2nasat 606 $aDesign optimization$2nasat 606 $aApproximation$2nasat 606 $aFlutter analysis$2nasat 606 $aInfluence coefficient$2nasat 606 $aPrediction analysis techniques$2nasat 606 $aUnsteady aerodynamics$2nasat 615 7$aMatrices (mathematics) 615 7$aTransonic flow. 615 7$aAerodynamic coefficients. 615 7$aDesign optimization. 615 7$aApproximation. 615 7$aFlutter analysis. 615 7$aInfluence coefficient. 615 7$aPrediction analysis techniques. 615 7$aUnsteady aerodynamics. 700 $aLi$b Wesley W$01405427 701 $aPak$b Chan-gi$f1956-$01395872 712 02$aHugh L. Dryden Flight Research Center. 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910701851203321 996 $aBasis function approximation of transonic aerodynamic influence coefficient matrix$93481897 997 $aUNINA