Use of High-Speed Microjets for Active Separation Control in Diffusers
Author:
Affiliation:
1. Florida A&M University and Florida State University, Tallahassee, Florida 32310
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.8552
Reference37 articles.
1. 3D subsonic diffuser design and analysis
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3. Design of the Blended Wing Body Subsonic Transport
4. Influence of inlet distortion on transonic compressor blade loading
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