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.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2307.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1985
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Format: Microform
Subjects: Cold surfaces.; Heat shielding.; Hypersonic flow.; Impingement.; Reusable heat shielding.; Thermal protection.; Tiles.; Turbulent boundary layer.; Turbulent flow.
Notes: "August 1985"--Cover.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1985] 1 microfiche.