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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/

Main Author:	Avery, Don E.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985
Series:	NASA technical paper 2307
Subjects:	Cold surfaces Heat shielding Hypersonic flow Impingement Reusable heat shielding Thermal protection Tiles Turbulent boundary layer Turbulent flow

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