Experimental Demonstration of Active Flow Control to Reduce Unsteady Stator-Rotor Interaction-Reference-Cited by-同舟云学术

Experimental Demonstration of Active Flow Control to Reduce Unsteady Stator-Rotor Interaction

Published:2001-03 Issue:3 Volume:39 Page:458-464
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Rao Nikhil M.¹,Feng Jinwei¹,Burdisso Ricardo A.¹,Ng Wing F.¹

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1327

Reference14 articles.

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2. 4Naumann, R. G. “Control of the Wake from a Simulated Blade by Trailing Edge Blowing,” M.S. Thesis,Dept. of Mechanical Engineering, Lehigh Univ., Bethlehem, PA,July 1992.

3. 5Corcoran, T. E. “Control of the Wake from a Simulated Blade by Trailing Edge Blowing,” M.S. Thesis,Dept. of Mechanical Engineering, Lehigh Univ., Bethlehem, PA,Jan. 1992.

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