Jet Direction Control Using Circular Cylinder with Tangential Blowing
Author:
Affiliation:
1. Graduate School of Mechanical Engineering, Kogakuin University
2. Department of Mechanical System Engineering, Kogakuin University
3. Department of Mechanical Engineering, Aoyama Gakuin University
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/64/3/64_T-20-26/_pdf
Reference21 articles.
1. 1) Englar, R. J. and Huson, G. G.: Development of Advanced Circulation Control Wing High-Lift Airfoils, J. Aircr., 21 (1984), pp. 476–483.
2. 2) Liu, Y., Sankar, L., Englar, R. J., and Ahuja, K.: Numerical Simulations of the Steady and Unsteady Aerodynamic Characteristics of a Circulation Control Wing Airfoil, 39th Aerospace Sciences Meeting and Exhibit, AIAA 2001-0704, 2001.
3. 3) Okamoto, T. and Yagita, M.: The Experimental Investigation on the Flow Past a Circular Cylinder of Finite Length Placed Normal to the Plane Surface in a Uniform Stream, Bull. JSME, 16, 95 (1973), pp. 805–814.
4. 4) De la Montanya, J. B. and Marshall, D.: Circulation Control and Its Application to Extreme Short Take-off and Landing Vehicles, 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2007-1404, 2007.
5. 5) Waka, R., Yoshino, F., Hayashi, T., and Iwasa, T.: The Aerodynamic Characteristics at the Mid-Span of a Circular Cylinder with Tangential Blowing, Bull. JSME, 26 (1983), pp. 755–762.
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1. Influence of Amplitude of Excited Secondary Flow on the Direction of Jets;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023
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