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100   $a19891113j197303    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe behavior of a compressible turbulent boundary layer in a shock-wave-induced adverse pressure gradient /$fby William C. Rose
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dMarch 1973.
215   $a1 online resource (vii, 229 pages) $cillustrations
225 1 $aNASA/TN ;$vD-7092
300   $a"March 1973."
320   $aIncludes bibliographical references (pages 90-95).
606   $aShock waves$2nasat
606   $aTurbulent boundary layer$2nasat
606   $aShock waves$2fast
606   $aPressure gradients$2nasat
606   $aTurbulent boundary layer$2fast
615  7$aShock waves.
615  7$aTurbulent boundary layer.
615  7$aShock waves.
615  7$aPressure gradients.
615  7$aTurbulent boundary layer.
700   $aRose$b William C.$f1940-$01401864
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aAmes Research Center.
712 02$aUniversity of Washington.
801  0$bABC
801  1$bABC
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801  2$bAD#
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801  2$bOCLCQ
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801  2$bGPO
906   $aBOOK
912   $a9910716669803321
996   $aThe behavior of a compressible turbulent boundary layer in a shock-wave-induced adverse pressure gradient$93471178
997   $aUNINA