journal article
Jul 01, 2018
Wind Tunnel Investigation of a Circulation Control Wing with Dual-Radius Flaps
Journal of Aircraft
Vol. 55
No. 4
pp. 1731-1741
·
American Institute of Aeronautics and Astronautics (AIAA)
Topics
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References
17
[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
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.
[6]
JenschC.PfingstenK. C.RadespielR. “Numerical Investigation of Leading Edge Blowing and Optimization of the Slot Geometry for a Circulation Control Airfoil,” Numerical and Experimental Fluid Mechanics VII, NNFM 112, Springer, Berlin, 2010, pp. 183–190. doi:10.1007/978-3-642-14243-7-23
[10]
Pankhurst R. C. (1952)
[11]
SchubauerG. B.SkramstadH. K. “Laminar Boundary Layer Oscillations and Stability of Laminar Flow,” NACA Rept. 909, 1948.
[12]
[13]
[14]
[15]
[16]
Blevins R. D. (2003)
[17]
Kanistras K. (2016)
Metrics
11
Citations
17
References
Details
- Published
- Jul 01, 2018
- Vol/Issue
- 55(4)
- Pages
- 1731-1741
Authors
Cite This Article
Konstantinos Kanistras, Pranith Chander Saka, Kimon P. Valavanis, et al. (2018). Wind Tunnel Investigation of a Circulation Control Wing with Dual-Radius Flaps. Journal of Aircraft, 55(4), 1731-1741. https://doi.org/10.2514/1.c034208
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