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Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10 / by J. David Dearing.
Connect to full text Available online
View online- Format:
- Book
- Government document
- Author/Creator:
- Dearing, J. David, author.
- Series:
- NASA technical note ; D-5146.
- NASA technical note ; NASA TN D-5146
- Language:
- English
- Subjects (All):
- Cone--Hypersonic aerodynamics.
- Cone.
- Laminar flow.
- Aerodynamic heating.
- Heat--Transmission.
- Heat.
- Space vehicles--Thermodynamics.
- Space vehicles.
- heat transmission.
- Physical Description:
- 1 online resource (20 pages) : illustrations.
- Place of Publication:
- Washington, D.C. : National Aeronautics and Space Administration, April 1969.
- Notes:
- "April 1969."
- Includes bibliographical references (page 9).
- Description based on online resource, PDF version; title from title page (NASA, viewed on Oct. 26, 2020).
- Other Format:
- Print version: Dearing, J. David. Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10.
- OCLC:
- 785286727
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