LEADER 01327nam--2200421---450- 001 990001678230203316 005 20050902173148.0 010 $a3-631-33479-6 035 $a000167823 035 $aUSA01000167823 035 $a(ALEPH)000167823USA01 035 $a000167823 100 $a20040519d1998----km-y0enga50------ba 101 $ager 102 $aDE 105 $a||||||||001yy 200 1 $aUntersuchungen zur alteren nordischen und germanischen Sprachgeschichte$fOttar Gronvik 210 $aFrankfurt am Main [etc.]$cP. Lang$d1998 215 $a178 p.$d21 cm. 225 2 $aOsloer Beitrage zur Germanistik$v18 410 0$12001$aOsloer Beitrage zur Germanistik$v18 454 1$12001 461 1$1001-------$12001 606 0 $aLinguistica comparativa 606 0 $aLingua tedesca 606 0 $aLingue scandinave 676 $a430.09021 700 1$aGRONVIK,$bOttar$0561997 801 0$aIT$bsalbc$gISBD 912 $a990001678230203316 951 $aIV.2. 1262 (XII E 95)$b174702 L.M.$cXII E$d00135123 959 $aBK 969 $aUMA 979 $aMARIA$b10$c20040519$lUSA01$h0934 979 $aRIVELLI$b90$c20050902$lUSA01$h1730 979 $aRIVELLI$b90$c20050902$lUSA01$h1731 996 $aUntersuchungen zur alteren nordischen und germanischen Sprachgeschichte$9941491 997 $aUNISA LEADER 01834oam 2200529 450 001 9910706548703321 005 20171201101145.0 035 $a(CKB)5470000002456961 035 $a(OCoLC)862774214 035 $a(EXLCZ)995470000002456961 100 $a20131110j200103 ua 0 101 0 $aeng 135 $aurbn||||a|a|| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /$fDavid M. Schuster 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMarch 2001. 215 $a1 online resource (37 pages) $cillustrations 225 1 $aNASA/TM ;$v2001-210828 300 $a"March 2001." 300 $a"Performing organization: NASA Langley Research Center"--Report documentation page. 320 $aIncludes bibliographical references (page 37). 606 $aTransonic wind tunnels$2nasat 606 $aAerodynamic characteristics$2nasat 606 $aDynamic pressure$2nasat 606 $aStatic pressure$2nasat 606 $aViscous flow$2nasat 606 $aWind tunnel tests$2nasat 615 7$aTransonic wind tunnels. 615 7$aAerodynamic characteristics. 615 7$aDynamic pressure. 615 7$aStatic pressure. 615 7$aViscous flow. 615 7$aWind tunnel tests. 700 $aSchuster$b D. M$g(David M.),$01413984 712 02$aLangley Research Center, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCO 801 2$bOCLCF 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910706548703321 996 $aAerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel$93511940 997 $aUNINA