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Displaying 1-1 of 1 results for author "Dillon, James L."
Aerodynamic characteristics of a hypersonic research airplane concept having a 70̊ swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 / Jim A. Penland, James B. Hallissy, and James L. Dillon.
- Text
- Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1979.
- 1979-12
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo52191
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