Fluidic Flow Control Effectors for Flight Control-Reference-Cited by-同舟云学术

Fluidic Flow Control Effectors for Flight Control

Published:2018-10 Issue:10 Volume:56 Page:3808-3824
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Warsop Clyde¹,Crowther William J.²

Affiliation:

1. BAE SYSTEMS Air, Bristol, England BS34 7QW, United Kingdom

2. The University of Manchester, Manchester, England M13 9PL, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056787

Reference67 articles.

1. EnglarR. J. “Experimental Investigation of the High Velocity Coanda Wall Jet Applied to Bluff Trailing Edge Circulation Control Airfoils,” David W. Taylor Naval Ship Research and Development Center, Rept. 4708, Bethesda, 1975.

2. EnglarR. J. “Two-Dimensional Transonic Wind Tunnel Tests of Three 15-Percent Thick Circulation Control Airfoils,” Rept. DTNSRDC/ASED-79/07, David W. Taylor Naval Ship Research and Development Center, Washington, D.C. 1970.

3. Design of the Circulation Control Wing STOL Demonstrator Aircraft

4. Circulation control pneumatic aerodynamics: blown force and moment augmentation and modification - Past, present and future

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