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
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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- Washington, D.C. National Aeronautics and Space Administration 1985
- 48 p.
- NASA TP 2307 : 1985 .
Space shuttle, Hypersonic flow, Thermal protection, Reusable surface, Impingement heating
LNASA TP 2307 : 1985
Space shuttle, Hypersonic flow, Thermal protection, Reusable surface, Impingement heating
LNASA TP 2307 : 1985