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

An edition of 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 (1985)

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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Publish Date

1985

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch,For sale by the National Technical Information Service]

Language

eng

Pages

Description:

subjects: Cold surfaces, Heat shielding, Hypersonic flow, Impingement, Reusable heat shielding, Thermal protection, Tiles, Turbulent boundary layer, Turbulent flow