LEADER 00682nam a2200229 u 4500 001 991004270137007536 005 20230403173549.0 008 230403s1975 it a r 001 0 ita d 040 $aBibl. Interfacoltà T. Pellegrino$bita 041 0 $aita 082 0 $a794.1 100 1 $aKarpov, Anatolij$059483 245 10$aScacchi primo amore /$cA. Karpov, A. Roscial 260 $aMilano :$bTeti editore,$c1975 300 $a235 p. :$bill. ;$c21 cm 500 $aTrad. di Edi Pietro Bozza e Zoia Kasianova 650 0$aScacchi 650 0$aPartite a scacchi 700 1 $aRoscial, Aleksandr 912 $a991004270137007536 996 $aScacchi primo amore$93377005 997 $aUNISALENTO 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