LEADER 01714oam  2200529   450 
001 9910716571203321
005 20210614094037.0
035   $a(CKB)5470000002522442
035   $a(OCoLC)785167531
035   $a(EXLCZ)995470000002522442
100   $a20120408j197210    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExperimental study of nozzle wall boundary layers at Mach numbers 20 to 47 /$fby Joseph H. Kemp and F. Kevin Owen
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dOctober 1972.
215   $a1 online resource (vii, 101 pages) $cillustrations
225 1 $aNASA/TN ;$vD-6965
300   $a"October 1972."
320   $aIncludes bibliographical references (pages 17-21).
606   $aJet nozzles$2nasat
606   $aTurbulent boundary layer$2nasat
606   $aWall pressure$2nasat
606   $aWall pressure (Aerodynamics)
606   $aAerodynamics, Hypersonic
615  7$aJet nozzles.
615  7$aTurbulent boundary layer.
615  7$aWall pressure.
615  0$aWall pressure (Aerodynamics)
615  0$aAerodynamics, Hypersonic.
700   $aKemp$b Joseph H.$01402441
702   $aOwen$b F. Kevin
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bCOP
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910716571203321
996   $aExperimental study of nozzle wall boundary layers at Mach numbers 20 to 47$93472911
997   $aUNINA