Transonic flow separation control by MEMS sensors and actuators-Reference-Cited by-同舟云学术

Transonic flow separation control by MEMS sensors and actuators

Published:2001-01-08 Issue: Volume: Page:
ISSN:
Container-title:39th Aerospace Sciences Meeting and Exhibit
language:
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Author:

Tung Steve¹,Maines Brant²,Jiang Fukang³,Tsao Tom³

Affiliation:

1. Arkansas, Univ., Fayetteville

2. Lockheed Martin Aeronautics Co., Fort Worth, TX

3. Umachines, Inc., Pasadena, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-123

Reference12 articles.

1. Taylor, H.D., 1947, "The Elimination of Diffuser Separation by Vortex Generators," UAC Research Department ReportR-4012-3.

2. Lin, J.C., Robinson, S.K., McGhee, R.J., and Valarezo, W.O., 1994, "Separation Control on High-Lift Airfoils via Micro-Vortex Generators," Journal ofAircraft, 31, No.6,Nov-Dec.

3. Lin, J.C., Selby, G.V., and Howard, F.G., 1991, "Exporatory Study of Vortex-Generating Devices for Turbulent Flow," AIAA-91-0042, 29thAerospace SciencesMeeting,Reno, January.

4. Pearcy, H.H., Rao, K., and Sykes, D.M. 1993, "Inclined Air-Jets used as Vortex Generators to Suppress Shock-Induced Separation," AGARDCP-534, Computational and Experimental Jets in crossFlow,November.

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