Vortex generator installation studies on steady state and dynamic inlet distortion

Author:

Anderson Bernhard1,Gibb James2

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. Defence Research Agency, Bedford, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

1. Bowditeh, D. N. and Cpltrin, R. E. "A Survey of Inlet/ EngineDistortionCompatibility,"AIAAPaperNo.83-1166, 1986.

2. Gibb,J,andJackson,M."SomePreliminary ResultsFrom Tests Using Vortex Generators in the Circular/Circular Diffusing S-Duct Model M Report AP4(92)WP15, Aug. 1992.

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