LEADER 00974nam0-22003131--450- 001 990009591260403321 005 20120614141152.0 010 $a3261013672 035 $a000959126 035 $aFED01000959126 035 $a(Aleph)000959126FED01 035 $a000959126 100 $a20120614d1974----km-y0itay50------ba 101 0 $ager 102 $aDE 105 $ay-------001yy 200 1 $a<>Streit um den Strafzweck zur Zeit der Weimarer Republik$fRalf Seidl 210 $aBern$cH. Lang$aFrankfurt am Main$cP. Lang$d1974 215 $a[5], XX, 226, [77] p.$d21 cm 225 1 $aEuropäische Hochschulschriften$hReihe 2$iRechtswissenschaft$v0094 676 $a340.43$v11 rid.$zita 700 1$aSeidl,$bRalf$0516904 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990009591260403321 952 $aX O 87 (94)$b111254$fFGBC 959 $aFGBC 996 $aStreit um den Strafzweck zur Zeit der Weimarer Republik$9844731 997 $aUNINA LEADER 02474oam 2200709 450 001 9910716019303321 005 20210601100647.0 035 $a(CKB)5470000002517915 035 $a(OCoLC)23295306$z(OCoLC)760971134 035 $a(EXLCZ)995470000002517915 100 $a19910326j197212 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aEffect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration /$fby Louis E. Clark 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1972. 215 $a1 online resource (52 pages) $cillustrations 225 1 $aNASA/TN ;$vD-7060 300 $a"December 1972." 320 $aIncludes bibliographical references (page 10). 606 $aAerospace vehicles$2nasat 606 $aAerodynamics$2nasat 606 $aSpace vehicles$xAtmospheric entry 606 $aLeading edges (Aerodynamics) 606 $aAerodynamic heating 606 $aAerothermodynamics 606 $aSpace shuttles 606 $aAerodynamic heating$2fast 606 $aAerothermodynamics$2fast 606 $aLeading edges (Aerodynamics)$2fast 606 $aSpace shuttles$2fast 606 $aSpace vehicles$xAtmospheric entry$2fast 615 7$aAerospace vehicles. 615 7$aAerodynamics. 615 0$aSpace vehicles$xAtmospheric entry. 615 0$aLeading edges (Aerodynamics) 615 0$aAerodynamic heating. 615 0$aAerothermodynamics. 615 0$aSpace shuttles. 615 7$aAerodynamic heating. 615 7$aAerothermodynamics. 615 7$aLeading edges (Aerodynamics) 615 7$aSpace shuttles. 615 7$aSpace vehicles$xAtmospheric entry. 700 $aClark$b Louis E.$01419962 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bABC 801 1$bABC 801 2$bAD# 801 2$bOCLCE 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCQ 801 2$bOCLCO 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910716019303321 996 $aEffect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration$93536156 997 $aUNINA