journal article
Sep 01, 1994
Application of Circulation Control to Advanced Subsonic Transport Aircraft, Part I - Airfoil Development
Journal of Aircraft
Vol. 31
No. 5
pp. 1160-1168
·
American Institute of Aeronautics and Astronautics (AIAA)
Topics
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References
27
[1]
Englar R. J. (1984)
[2]
Englar R. J. (1975)
[3]
Mones, D. G. "Measurements of Wall Jet Development on a Circulation Control Aerofoil," Ph.D. Dissertation, Mechanical Engineering Dept.Univ. of California, Davis, Davis, CA,Jan. 1971.
[4]
Englar R. J. (1971)
[5]
Englar R. J. (1979)
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Englar R. J. (1981)
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Englar R. J. (1847)
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Wilson M. B. (1979)
[10]
Englar R. J. (1842)
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[12]
Englar R. J. Canadian Aeronautics and Space Journal (1973)
[13]
Englar R. J. (1991)
[14]
Englar R. J. (1988)
[15]
15Kohlman, D. L., Introduction to VISTOL Airplanes, Iowa State Univ. Press, Ames, IA, 1981, pp.123-165.
[16]
Gibbs E. H. (1975)
[17]
[18]
[19]
Dash S. M. (1982)
[20]
[21]
[22]
Pulliam T. H. (1985)
[23]
23Wu, J.C, "A Study of Unsteady Turbulent Flow Past Airfoils," Ph.D. Dissertation, Georgia Inst. of Technology, Atlanta,GA, June 1988.
[24]
[25]
Smith M. J. (1990)
[26]
26Shrewsbury, G. D. "Dynamic Stall of Circulation Control Airfoils," Ph.D. Dissertation, Georgia Inst. of Technology, Atlanta,GA, Nov. 1990.
10.2514/6.1990-573
[27]
Englar R. J. (1991)
Metrics
62
Citations
27
References
Details
- Published
- Sep 01, 1994
- Vol/Issue
- 31(5)
- Pages
- 1160-1168
Authors
Cite This Article
Robert J. Englar, Marilyn J. Smith, Sean M. Kelley, et al. (1994). Application of Circulation Control to Advanced Subsonic Transport Aircraft, Part I - Airfoil Development. Journal of Aircraft, 31(5), 1160-1168. https://doi.org/10.2514/3.56907
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