LEADER 01815oam 2200601I 450 001 9910715060003321 005 20201117110353.0 035 $a(CKB)5470000002507403 035 $a(OCoLC)760892609 035 $a(EXLCZ)995470000002507403 100 $a20111113j196809 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aEffects of boundary layer buildup in shock tubes upon chemical rate measurements /$fby Marvin Warshay 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dSeptember 1968. 215 $a1 online resource (ii, 15 pages) $cillustrations 225 1 $aNASA technical note ;$vTN D-4795 300 $a"September 1968." 320 $aIncludes bibliographical references (page 15). 606 $aBoundary layer 606 $aAerodynamics 606 $aShock tubes 606 $aBromine 606 $aAerodynamics$2fast 606 $aBoundary layer$2fast 606 $aBromine$2fast 606 $aShock tubes$2fast 615 0$aBoundary layer. 615 0$aAerodynamics. 615 0$aShock tubes. 615 0$aBromine. 615 7$aAerodynamics. 615 7$aBoundary layer. 615 7$aBromine. 615 7$aShock tubes. 700 $aWarshay$b Marvin$01399369 712 02$aUnited States.$bNational Aeronautics and Space Administration, 712 02$aLewis Research Center. 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCA 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910715060003321 996 $aEffects of boundary layer buildup in shock tubes upon chemical rate measurements$93545448 997 $aUNINA