LEADER 00917nam a2200265 i 4500 001 991001285049707536 005 20020507113849.0 008 970308s1986 it ||| | ita 020 $a8870564053 035 $ab10199214-39ule_inst 035 $aLE00645207$9ExL 040 $aDip.to Fisica$bita 084 $a005.369 084 $a621.3.8 110 2 $aLotus Development Corporation$0464203 245 10$aSymphony :$bla grande guida /$cLotus Development Corporation 260 $aMilano :$bGruppo Editoriale Jackson,$c1986 300 $av, 432 p. ;$c24 cm. 650 4$aMicroelaboratori elettronici-Programmi 907 $a.b10199214$b21-09-06$c27-06-02 912 $a991001285049707536 945 $aLE006 621.3.8 LOT$g1$i2006000051453$lle006$o-$pE0.00$q-$rl$s- $t0$u0$v0$w0$x0$y.i10245972$z27-06-02 996 $aSymphony$9190920 997 $aUNISALENTO 998 $ale006$b01-01-97$cm$da $e-$fita$git $h0$i1 LEADER 01691nam 2200505I 450 001 9910702734603321 005 20150203132632.0 035 $a(CKB)5470000002430855 035 $a(OCoLC)902680759 035 $a(EXLCZ)995470000002430855 100 $a20150203j201408 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aData reduction functions for the Langley 14- by 22-foot subsonic tunnel /$fAndy D. Boney 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dAugust 2014. 215 $a1 online resource (iii, 77 pages) 225 1 $aNASA/TM ;$v2014-218513 300 $aTitle from title screen (viewed Feb. 3, 2015). 300 $a"August 2014." 320 $aIncludes bibliographical references (page 77). 606 $aData reduction$2nasat 606 $aSubsonic wind tunnels$2nasat 606 $aFlowmeters$2nasat 606 $aJet exhaust$2nasat 606 $aWall pressure$2nasat 606 $aLoads (forces)$2nasat 615 7$aData reduction. 615 7$aSubsonic wind tunnels. 615 7$aFlowmeters. 615 7$aJet exhaust. 615 7$aWall pressure. 615 7$aLoads (forces) 700 $aBoney$b Andy D.$01405267 702 $aNishikawa$b Hiroaki 712 02$aLangley Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910702734603321 996 $aData reduction functions for the Langley 14- by 22-foot subsonic tunnel$93481437 997 $aUNINA