Wind Tunnel Investigation of a Circulation Control Wing with Dual-Radius Flaps-Reference-Cited by-同舟云学术

Wind Tunnel Investigation of a Circulation Control Wing with Dual-Radius Flaps

Published:2018-07 Issue:4 Volume:55 Page:1731-1741
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Kanistras Konstantinos¹,Saka Pranith Chander¹,Valavanis Kimon P.¹,Rutherford Matthew J.¹

Affiliation:

1. University of Denver Unmanned Systems Research Institute (DU2SRI), Denver, Colorado 80210

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034208

Reference17 articles.

1. EnglarR. J.WilliamsR. M. “Design of Circulation Controlled Stern Plane for Submarine Applications,” Rept. NSRDC/AL-200 (AD901-198), Naval Ship Research and Development Center, Bethesda, MD, March 1971.

2. EnglarR. J. “Overview of Circulation Control Pneumatic Aerodynamics: Blown Force and Moment Augmentation and Modification as Applied Primarily to Fixed-Wing Aircraft,” NASA CP-2005-213509/PTI, June 2005. doi:10.2514/5.9781600866838.0023.0068

3. EnglarR. J., Development of the A-6/Circulation Control Wing Flight Demonstrator Configuration, David W. Taylor Naval Ship Research and Development Center, Bethesda, MD, 1979, pp. 26–32.

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

5. Design and Performance of Circulation Control Flap Systems

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