Parametric study toward optimization of blowing and suction locations for improving lift-to-drag ratio on a Clark-Y airfoil

Author:

OHASHI Masahiro1,MORITA Yuki1,HIROKAWA Shiho1,FUKAGATA Koji1,TOKUGAWA Naoko2

Affiliation:

1. Department of Mechanical Engineering, Keio University

2. Aerospace Technology Directorate, Japan Aerospace Exploration Agency

Publisher

Japan Society of Mechanical Engineers

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering

Reference18 articles.

1. Abbas, A., De Vicente, J., and Valero, E., Aerodynamic technologies to improve aircraft performance, Aerosp. Sci. Technol., Vol. 28, No. 1 (2013), pp. 100–132.

2. Choi, H., Moin, P., and Kim, J., Direct numerical simulation of turbulent flow over riblets, J. Fluid. Mech., Vol. 255 (1993), pp. 503–539.

3. Eto, K., Kondo, Y., Fukagata, K., and Tokugawa, N., Friction drag reduction on a Clark-Y airfoil using uniform blowing, AIAA J., Vol. 57 (2019), pp. 2774–2782.

4. Farland, G., Flow control for turbulent skin-friction drag reduction on airfoils. Master Thesis, Karlsruhe Institute of Technology (2019).

5. Fukagata, K., Iwamoto, K., and Kasagi, N., Contribution of Reynolds stress distribution to the skin friction in wall-bounded flows, Phys. Fluids, Vol. 14 (2002), L73–L76.

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