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Heat-transfer and pressure distributions on hemisphere-cylinders in methane-air combustion products at Mach 7 / by Irving Weinstein.
- Format:
- Book
- Government document
- Author/Creator:
- Weinstein, Irving, author.
- Series:
- NASA technical note ; D-7104.
- NASA/TN ; D-7104
- Language:
- English
- Subjects (All):
- Aerodynamic heating.
- Heat--Transmission.
- Heat.
- Aerodynamics, Hypersonic.
- heat transmission.
- Aerodynamic load.
- Cylinders.
- Physical Description:
- 1 online resource (38 pages) : illustrations.
- Place of Publication:
- Washington, D.C. : National Aeronautics and Space Administration, January 1973.
- Summary:
- Heat-transfer and pressure distributions were measured over the surfaces of three hemisphere-cylinder models tested at a nominal Mach number of 7 in the Langley 8-foot high-temperature structures tunnel which uses methane-air products of combustion as a test medium. The results showed that the heat-transfer and pressure distributions over the surface of the models were in good agreement with experimental data obtained in air and also with theoretical predictions.
- Notes:
- "January 1973."
- Includes bibliographical references (pages 11-12).
- Description based on online resource, PDF version; title from title page (NASA, viewed on June 9, 2021).
- Other Format:
- Online version: Weinstein, Irving, https://id.oclc.org/worldcat/entity/E39PCjHkFkXGtV8w7drJYxjYdP. Heat-transfer and pressure distributions on hemisphere-cylinders in methane-air combustion products at Mach 7.
- OCLC:
- 23449212
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