Controlled Streamwise Vorticity in Diffuser Boundary Layer Using Hybrid Synthetic Jet Actuation-Reference-Cited by-同舟云学术

Controlled Streamwise Vorticity in Diffuser Boundary Layer Using Hybrid Synthetic Jet Actuation

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA Fluid Dynamics Conference
language:
Short-container-title:

Author:

Gissen Abraham¹,Vukasinovic Bojan¹,Glezer Ari¹

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-4021

Reference19 articles.

1. Separation Control in Duct Flows

2. Anabtawi, A.J., Blackwelder, R.F., Lissaman, B.S.P, Liebeck, R.H. "An Experimental Investigation of Boundary Layer ingestion in a Diffusing S-Duct With and Without Passive FlowControl,"AIAAPaper1999-0739,1999.

3. Study on vortex generator flow control for the management of inlet distortion

4. Anderson, B.H., Baust, D.H., Agrell, J. "Management of Total Pressure Recovery, Distortion and High Cycle Fatigue in CompactAirVehicleInlets,"NASA/TM.2002-212000.

5. Anderson, B.H., Miller, D.N., Addington, G.A., Agrell, J. "Optimal Micro-Vane Flow Control for Compact Air Vehicle Inlets,"NASA/TM.2004-212936.

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