Research Catalog
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Displaying 1-4 of 4 results
A numerical analysis applied to high angle of attack three-dimensional inlets [microform] / Danny P. Hwang.
- Text
- [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
- 1986
Effect of a rotating propeller on the separation angle of attack and distortion in ducted propeller inlets [microform] / D. R. Boldman, ... [et al.].
- Text
- [Washington, DC] : National Aeronautics and Space Administration, [1992?]
- 1992
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS97761Subsonic high-angle-of-attack aerodynamic characteristics of a cone and cylinder with triangular cross sections and a cone with a square cross section [microform] / Mark H. Clarkson ... [et al.].
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
- 1983
Tables for supersonic flow around right circular cones at zero angle of attack / by Joseph L. Sims.
- Text
- Washington, DC : Office of Scientific and Technical Information, NASA. 1964.
- 1964
- 1 Item
Item details Format Call Number Item Location Text 92514.858 Off-site
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