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035   $a(CKB)5470000002517294
035   $a(OCoLC)150483928$z(OCoLC)761215476
035   $a(EXLCZ)995470000002517294
100   $a19871030j196901    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5° half-angle cone at Mach 8 /$fby P. Calvin Stainback
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dJanuary 1969.
215   $a1 online resource (76 pages) $cillustrations
225 1 $aNASA/TN ;$vD-4961
300   $a"January 1969."
320   $aIncludes bibliographical references (pages 24-27).
606   $aReynolds number$2nasat
606   $aAerodynamics$2nasat
606   $aMach number$2nasat
606   $aAerodynamics, Hypersonic
606   $aAerodynamics, Hypersonic$2fast
606   $aAngle of attack (Aerodynamics)$2fast
606   $aNoses (Space vehicles)$2fast
606   $aReynolds number$2fast
615  7$aReynolds number.
615  7$aAerodynamics.
615  7$aMach number.
615  0$aAerodynamics, Hypersonic.
615  7$aAerodynamics, Hypersonic.
615  7$aAngle of attack (Aerodynamics)
615  7$aNoses (Space vehicles)
615  7$aReynolds number.
700   $aStainback$b P. Calvin$01401641
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bUAU
801  1$bUAU
801  2$bEGM
801  2$bAD#
801  2$bOCLCE
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716080803321
996   $aEffect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5° half-angle cone at Mach 8$93470598
997   $aUNINA