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 View on Open Library

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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First published: 1985 1 language
Subjects
Cold surfaces Heat shielding Hypersonic flow Impingement Reusable heat shielding Thermal protection Tiles Turbulent boundary layer Turbulent flow

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