LEADER 01350nam2-2200397li-450 001 990000199460203316 005 20180312154828.0 010 $a0-7923-9375-9 035 $a0019946 035 $aUSA010019946 035 $a(ALEPH)000019946USA01 035 $a0019946 100 $a2001994091993-------y0itay0103----ba 101 0 $aeng 102 $aUS 200 1 $aEffective polynomial computational$fby Richard Zippel 210 $aBoston [etc.]$cKluwer Academic Publishers$dcopyr. 1993 215 $aXI, 363 p.$cill.$d24 cm 225 2 $a<> Kluwer international series inengineering and computer science$v241 410 0$10010019941$12001$a<> Kluwer international series inengineering and computer science 610 1 $aalgoritmi 610 1 $aelaborazione elettronica$amodelli matematici 610 1 $apolinomi 700 1$aZippel,$bRichard E.$0754445 801 $aSistema bibliotecario di Ateneo dell' Università di Salerno$gRICA 912 $a990000199460203316 951 $a512.9 ZIP$b16180/CBS$c512.9$d00220147 959 $aBK 969 $aSCI 979 $c19940919 979 $c20001110$lUSA01$h1713 979 $c20020403$lUSA01$h1627 979 $aPATRY$b90$c20040406$lUSA01$h1614 979 $aRSIAV6$b90$c20090512$lUSA01$h1037 996 $aEffective polynomial computational$91518121 997 $aUNISA LEADER 01383oam 2200409 450 001 9910717190203321 005 20220118084509.0 035 $a(CKB)5470000002528310 035 $a(OCoLC)1292076425 035 $a(OCoLC)995470000002528310 035 $a(EXLCZ)995470000002528310 100 $a20220114j197705 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aDetermining the lift and drag distributions on a three-dimensional airfoil from flow-field velocity surveys /$fKenneth L. Orloff 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dMay 1977. 215 $a1 online resource (approximately 77 pages) $cillustrations 225 1 $aNASA TM ;$v73247 300 $a"May 1977." 606 $aAerodynamics$2nasat 606 $aAirfoils$2nasat 606 $aVelocity$2nasat 615 7$aAerodynamics. 615 7$aAirfoils. 615 7$aVelocity. 700 $aOrloff$b Kenneth L.$01419184 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 801 2$bGPO 906 $aBOOK 912 $a9910717190203321 996 $aDetermining the lift and drag distributions on a three-dimensional airfoil from flow-field velocity surveys$93532854 997 $aUNINA