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035   $a(CKB)5470000002464549
035   $a(OCoLC)956368950
035   $a(EXLCZ)995470000002464549
100   $a20160809j199612    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExperimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction /$fHyun D. Kim, Warren R. Hingst, and David O. Davis
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dDecember 1996.
215   $a1 online resource (9 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107392
300   $aTitle from title screen (viewed Aug. 9, 2016).
300   $a"December 1996"--Report documentation page.
300   $a"Prepared for the 35th Aerospace Sciences Meeting and Exhibit cosponsored by AIAA, ASME, SAE, and ASME, Reno, Nevada, January 6-10, 1997."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
300   $a"AIAA-97-0608."
320   $aIncludes bibliographical references (page 9).
606   $aBoundary layer control$2nasat
606   $aPressure measurement$2nasat
606   $aFlow visualization$2nasat
606   $aTurbulent boundary layer$2nasat
606   $aMass flow rate$2nasat
606   $aStatic pressure$2nasat
606   $aShock waves$2nasat
615  7$aBoundary layer control.
615  7$aPressure measurement.
615  7$aFlow visualization.
615  7$aTurbulent boundary layer.
615  7$aMass flow rate.
615  7$aStatic pressure.
615  7$aShock waves.
700   $aKim$b Hyun Dae$01390070
702   $aHingst$b Warren R.
702   $aDavis$b David O.
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707497503321
996   $aExperimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction$93442386
997   $aUNINA