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035   $a(OCoLC)1196870103
035   $a(EXLCZ)995470000002516976
100   $a20200922j196811    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffects of angle of attack and bluntness on the shock-layer properties of a 15°cone at Mach number of 10.6 /$fby Joseph W. Cleary
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dNovember 1968.
215   $a1 online resource (38 pages) $cillustrations
225 1 $aNASA/TN ;$vD-4909
300   $a"November 1968."
320   $aIncludes bibliographical references (page 11).
606   $aMach number$2nasat
606   $aAerodynamics$2nasat
606   $aConical shells$2fast
606   $aShock (Mechanics)$2fast
615  7$aMach number.
615  7$aAerodynamics.
615  7$aConical shells.
615  7$aShock (Mechanics)
700   $aCleary$b Joseph W.$01398111
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bCOP
801  1$bCOP
801  2$bOCLCF
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910715912303321
996   $aEffects of angle of attack and bluntness on the shock-layer properties of a 15°cone at Mach number of 10.6$93460765
997   $aUNINA