Numerical Study on Unsteady Flow Field Structure over Wing within Propeller Slipstream at Low-Reynolds-Number
Author:
Affiliation:
1. Graduate School of Engineering Science, Yokohama National University
2. Institute of Fluid Science, Tohoku University
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tastj/22/0/22_22.49/_pdf
Reference32 articles.
1. 1) Tani, I.: Low-Speed Flows Involving Bubble Separations, Prog. Aerosp. Sci., 5 (1964), pp. 70-103.
2. 2) Winslow, J., Otsuka, H., Govindarajan, B., and Chopra, I.: Basic Understanding of Airfoil Characteristics at Low Reynolds Numbers (104-105), J. Aircr., 55 (2018), pp. 1050-1061.
3. 3) Hain, R., Kahler, C. J., and Radespiel, R.: Dynamics of Laminar Separation Bubbles at Low-Reynolds-number Aerofoils, J. Fluid Mech., 630 (2009), pp. 129-153.
4. 4) Lambert, A. and Yarusevych, S.: Effect of Angle of Attack on Vortex Dynamics in Laminar Separation Bubbles, Phys. Fluids, 31 (2019), pp. 1-16.
5. 5) Fujita, K., Nagai, H., and Asai, K.: Conceptual Design of a Miniature, Propeller-Driven Airplane for Mars, AIAA Paper 2012-0847, 2012.
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