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Prediction of subsonic vortex shedding from forebodies with chines [microform] / Michael R. Mendenhall and Daniel J. Lesieutre.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
- 1990
Effects of forebody geometry on subsonic boundary-layer stability / S. S. Dodbele.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
- 1990
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS60902Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 / by Cornelius Driver.
- Text
- Washington : National Aeronautics and Space Administration, September 1959.
- 1959-9
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo182854
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