LEADER 01820oam 2200529 450 001 9910715978503321 005 20210331112634.0 035 $a(CKB)5470000002516307 035 $a(OCoLC)761308350 035 $a(EXLCZ)995470000002516307 100 $a20111115j196809 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aEquilibrium normal-shock and stagnation-point properties of helium for incident-shock Mach numbers from 1 to 30 /$fby Walter B. Olstad, Jane T. Kemper, and Roger D. Bengtson 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dSeptember 1968. 215 $a1 online resource (49 pages) $cillustrations 225 1 $aNASA/TN ;$vD-4754 300 $a"September 1968." 320 $aIncludes bibliographical references (page 16). 606 $aFluid mechanics$2nasat 606 $aMach number$2nasat 606 $aThermodynamic equilibrium$2nasat 606 $aThermodynamics$2nasat 606 $aHelium$xThermal properties$2fast 615 7$aFluid mechanics. 615 7$aMach number. 615 7$aThermodynamic equilibrium. 615 7$aThermodynamics. 615 7$aHelium$xThermal properties. 700 $aOlstad$b Walter B.$01417383 702 $aKemper$b Jane T. 702 $aBengtson$b Roger D. 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCO 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910715978503321 996 $aEquilibrium normal-shock and stagnation-point properties of helium for incident-shock Mach numbers from 1 to 30$93525544 997 $aUNINA