LEADER 02628oam 2200745I 450 001 9910709616703321 005 20180612110006.0 035 $a(CKB)5470000002472073 035 $a(OCoLC)761382490 035 $a(OCoLC)995470000002472073 035 $a(EXLCZ)995470000002472073 100 $a20111115j198501 ua 0 101 0 $aeng 135 $aurun||||a|a|| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes /$fRobert J. Nowak, Cindy W. Albertson, and L. Roane Hunt 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dJanuary 1985. 215 $a1 online resource (87 pages) $cillustrations 225 1 $aNASA/TP ;$v2345 300 $a"January 1985." 300 $aPrepared at Langley Research Center. 320 $aIncludes bibliographical references (pages 19-21). 606 $aFlow distribution$2nasat 606 $aCones$2nasat 606 $aAerodynamic heating$2nasat 606 $aBoundary layer transition$2nasat 606 $aTurbulent boundary layer$2nasat 606 $aAngle of attack (Aerodynamics) 606 $aNoses (Aircraft) 606 $aReynolds number 606 $aAerothermodynamics 606 $aAerothermodynamics$2fast 606 $aAngle of attack (Aerodynamics)$2fast 606 $aNoses (Aircraft)$2fast 606 $aReynolds number$2fast 615 7$aFlow distribution. 615 7$aCones. 615 7$aAerodynamic heating. 615 7$aBoundary layer transition. 615 7$aTurbulent boundary layer. 615 0$aAngle of attack (Aerodynamics) 615 0$aNoses (Aircraft) 615 0$aReynolds number. 615 0$aAerothermodynamics. 615 7$aAerothermodynamics. 615 7$aAngle of attack (Aerodynamics) 615 7$aNoses (Aircraft) 615 7$aReynolds number. 700 $aNowak$b Robert J.$01401795 702 $aAlbertson$b Cindy W. 702 $aHunt$b L. Roane$g(Lewis Roane), 712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCO 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910709616703321 996 $aAerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes$93470994 997 $aUNINA