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].
- Physical Description: 1 online resource (iii, 262 pages) : illustrations.
- Publisher: Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, December 1996.
|General Note:|| Title from title screen (viewed March 2, 2016).
"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
|Bibliography, etc. Note:|| Includes bibliographical references (page 262).
|Funding Information Note:|| Sponsored by the National Aeronautics and Space Administration WU 505-59-53-05 L-17443
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