LEADER 00783nam0-22002891i-450- 001 990008014790403321 005 20050301110236.0 010 $a0-521-01084-5 035 $a000801479 035 $aFED01000801479 035 $a(Aleph)000801479FED01 035 $a000801479 100 $a20050301d2002----km-y0itay50------ba 101 $aeng 105 $ay-------001yy 200 1 $aChaos in Dynamical Systems$fEdward Ott 205 $a2nd 210 $aCambridge$cCambridge University Press$d2002 215 $aXI, 478 p.$cill.$d25 cm 700 1$aOtt,$bEdward$021406 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990008014790403321 952 $a04 014-73$bDIC 4238$fDINCH 959 $aDINCH 996 $aChaos in dynamical systems$947605 997 $aUNINA LEADER 01891oam 2200601 450 001 9910706179903321 005 20170823100541.0 035 $a(CKB)5470000002454625 035 $a(OCoLC)858260762 035 $a(EXLCZ)995470000002454625 100 $a20130912j199905 ua 0 101 0 $aeng 135 $aurbn||||a|a|| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 12$aA parametric study of accelerations of an airplane due to a wake vortex system /$fEric C. Stewart 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMay 1999. 215 $a1 online resource (36 pages) $cillustrations 225 1 $aNASA/TM ;$v1999-208745 300 $a"May 1999." 300 $a"Performing organization: NASA Langley Research Center"--Report documentation page. 320 $aIncludes bibliographical references (page 15). 606 $aAerodynamics$2nasat 606 $aFlow distribution$2nasat 606 $aRectangular wings$2nasat 606 $aRoll$2nasat 606 $aRotation$2nasat 606 $aVortices$2nasat 606 $aYaw$2nasat 606 $aAircraft wakes$2nasat 606 $aMathematical models$2nasat 615 7$aAerodynamics. 615 7$aFlow distribution. 615 7$aRectangular wings. 615 7$aRoll. 615 7$aRotation. 615 7$aVortices. 615 7$aYaw. 615 7$aAircraft wakes. 615 7$aMathematical models. 700 $aStewart$b Eric C.$01395238 712 02$aLangley Research Center, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCO 801 2$bOCLCF 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910706179903321 996 $aA parametric study of accelerations of an airplane due to a wake vortex system$93453417 997 $aUNINA