Research Catalog
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Displaying 1-4 of 4 results
Three dimensional solution of pneumatic active control of forebody vortex asymmetry [microform] / Osama A. Kandil and Hazem H. Sharaf El-Din, C.H. Liu.
- Text
- Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Computational investigation of tangential slot blowing on a generic chined forebody [microform] / Roxana M. Agosta-Greenman ... [et al.].
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Effect of curvature on the impact damage characteritiscs and residual strength of composite plates [microform] / Damodar R. Ambur and James H. Starnes, Jr.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
- 1998
Experiments in aircraft roll-yaw control using forebody tangential blowing [microform] / Nelson Pedreiro.
- Text
- [Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
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