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Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7 — ReaderExpo

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Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7

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Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7

by Don E. Avery

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Cold surfacesHeat shieldingHypersonic flowImpingementReusable heat shieldingThermal protectionTilesTurbulent boundary layerTurbulent flow

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