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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aInvestigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds /$fby Mary W. Jackson and K.R. Czarnecki
210  1$aWashington :$cNational Aeronautics and Space Administration,$dApril 1960.
215   $a1 online resource (16 pages) $cillustrations
225 1 $aNASA technical note ;$vD-242
300   $a"April 1960."
320   $aIncludes bibliographical references (page 8).
606   $aReynolds number$2fast
606   $aTurbulence$2fast
606   $aConical bodies$2nasat
606   $aReynolds number$2nasat
606   $aSupersonic boundary layers$2nasat
606   $aSurface roughness effects$2nasat
606   $aTransition points$2nasat
606   $aTurbulent boundary layer$2nasat
606   $aTurbulent flow$2nasat
606   $aWind tunnel tests$2nasat
606   $aSchlieren photography$2nasat
606   $aSupersonic speed$2nasat
606   $aWind tunnel models$2nasat
615  7$aReynolds number.
615  7$aTurbulence.
615  7$aConical bodies.
615  7$aReynolds number.
615  7$aSupersonic boundary layers.
615  7$aSurface roughness effects.
615  7$aTransition points.
615  7$aTurbulent boundary layer.
615  7$aTurbulent flow.
615  7$aWind tunnel tests.
615  7$aSchlieren photography.
615  7$aSupersonic speed.
615  7$aWind tunnel models.
700   $aJackson$b Mary W.$01419784
702   $aCzarnecki$b K. R.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
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996   $aInvestigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds$93535473
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