Suppression of Cavity Loads Using Leading Edge Blowing Concepts

Author:

Arunajatesan Srinivasan1,Kannepalli Chandrasekhar1,Sinha Neeraj1,Sheehan Michael2,Shumway George3

Affiliation:

1. Combustion Research and Flow Technology, Inc

2. Florida A&M and Florida State University

3. Department of Mechanical and Aerospace Engineering University of Florida

Publisher

American Institute of Aeronautics and Astronautics

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Studies on the Influence of Steady Microactuators on Shock-Wave/Boundary-Layer Interaction;AIAA Journal;2013-12

2. Generation and Control of Oblique Shocks Using Microjets;AIAA Journal;2011-12

3. Studies on the Control of Shock Wave-Boundary layer Interaction Using Steady Microactuators;41st AIAA Fluid Dynamics Conference and Exhibit;2011-06-14

4. Flowfield Characteristics of Oblique Shocks Generated Using Microjet Arrays;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

5. Virtual Shock Shaping Using Microjet Arrays;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

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