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Numerical analysis of a variable camber rotor blade as a lift cotrol device [microform] / Alfred O. Awani [and] Robert H. Stroub.
- Text
- Lawrence, Kans : Flight Research Laboratory, University of Kansas Center for Research, Inc. ; [Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, 1984]
- 1984
Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads [microform] / John T. Batina.
- Text
- Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
- 1985
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS96402
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