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Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber / S. Naomi McMillin [and five others].
- Format:
- Book
- Government document
- Author/Creator:
- McMillin, S. Naomi (Susan Naomi), author.
- Series:
- NASA technical memorandum ; 4673.
- NASA technical memorandum ; 4673
- Language:
- English
- Subjects (All):
- Flow visualization.
- Reynolds number.
- Physical Description:
- 1 online resource (iii, 262 pages) : illustrations.
- Place of Publication:
- Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, December 1996.
- Notes:
- Title from title screen (viewed March 2, 2016).
- "December 1996."
- "Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
- Includes bibliographical references (page 262).
- Other Format:
- Print version: Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber
- Microfiche version: Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber
- OCLC:
- 942651780
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