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Effect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4 / by H. Harris Hamilton, and J. David Dearing.
- Format:
- Book
- Government document
- Author/Creator:
- Hamilton, H. Harris, author.
- Dearing, J. David, author.
- Series:
- NASA technical note ; D-4686.
- NASA technical note ; TN D-4686
- Language:
- English
- Subjects (All):
- Boundary layer control.
- Flaps (Airplanes).
- Wedges.
- Aircraft separation.
- wedges.
- Physical Description:
- 1 online resource (44 pages) : illustrations.
- Place of Publication:
- Washington, D.C. : National Aeronautics and Space Administration, August 1968.
- Notes:
- "August 1968."
- Includes bibliographical references (pages 18-21).
- Description based on online resource, PDF version; title from title page (NASA, viewed on Dec. 11, 2020).
- Electronic reproduction. [Place of publication not identified]: HathiTrust Digital Library. 2024.
- Other Format:
- Print version: Hamilton, H. Harris. Effect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4.
- OCLC:
- 761497571
- Access Restriction:
- Use copy Restrictions unspecified
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