02456oam 2200745 450 991071536230332120210420112149.0(CKB)5470000002510410(OCoLC)761237517(OCoLC)995470000002510410(EXLCZ)99547000000251041020111115j196004 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierInvestigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds /by Mary W. Jackson and K.R. CzarneckiWashington :National Aeronautics and Space Administration,April 1960.1 online resource (16 pages) illustrationsNASA technical note ;D-242"April 1960."Includes bibliographical references (page 8).Reynolds numberfastTurbulencefastConical bodiesnasatReynolds numbernasatSupersonic boundary layersnasatSurface roughness effectsnasatTransition pointsnasatTurbulent boundary layernasatTurbulent flownasatWind tunnel testsnasatSchlieren photographynasatSupersonic speednasatWind tunnel modelsnasatReynolds number.Turbulence.Conical bodies.Reynolds number.Supersonic boundary layers.Surface roughness effects.Transition points.Turbulent boundary layer.Turbulent flow.Wind tunnel tests.Schlieren photography.Supersonic speed.Wind tunnel models.Jackson Mary W.1419784Czarnecki K. R.United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCOOCLCFOCLCQGPOOCLCOGPOBOOK9910715362303321Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds3535473UNINA