Measurement of skin friction distribution using oil film for industrial wind tunnels
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, Aerodynamics Research Unit
Publisher
The Visualization Society of Japan
Link
https://www.jstage.jst.go.jp/article/tvsj/41/9/41_28/_pdf
Reference23 articles.
1. 1) J. W. Naughton, Mark Sheplak, “Modern developments in shear stress measurement” Progress in Aerospace Sciences 38 (2002) 515-570, 2002.
2. 2) Christopher Marks, Rolf Sondergaard and Mitch Wolff, “Surface Stress Sensitive Film as a Separation Control Sensor”, AIAA Paper 2012-0746, 2012.
3. 3) T.Gunnar Johansson, Faraz Mehdi, Jonathan W Naughton, “Some Problems with Near-Wall Measurements and the Determination of Wall Shear Stress” AIAA Paper 2006-3833, 2006.
4. 4) Yoshida, K., “Supersonic Drag Reduction Technology in the Scaled Supersonic Experimental Airplane Project by JAXA”, Progress in Aerospace Sciences, Vol.45, pp.124-146.
5. 5) Tokugawa, N., Kwak, D., Yoshida, K., Ueda, Y., “Transition Measurement of Natural Laminar Flow Wing on Supersonic Experimental Airplane (NEXST-1)”, Journal of Aircraft, Vol.45, No.5, pp1495-1504, 2008.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Measurement of Fluid Friction Acting on Flat Plate;Springer Proceedings in Physics;2024
2. Measurement of Shear Stress Acting on Flat Plate Using Oil Film Interferometry;Open Journal of Fluid Dynamics;2023
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