Ring-Force Balance System for Small Wind Tunnels
Author:
Affiliation:
1. Department of Aerospace Engineering, Nagoya University
2. Department of Mechanical and Aerospace Engineering, Tottori University
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tastj/13/0/13_TJSAS-D-14-00114/_pdf
Reference6 articles.
1. 1) Pole, A. and Kennith, L. G.: High-speed Wind Tunnel Testing, John Wiley & Sons, Inc., (1965).
2. 2) Vlluz, R. J.: Handbook of Supersonic Aerodynamics, Section 20, Wind Tunnel Instrumentation and Operation, Navord Report 1488, 6, (1961).
3. 3) Ewald, B. F. R.: Multi-component Force Balance for Conventional and Cryogenic Wind Tunnel, Meas. Sci. Technol., 11, (2000), pp. R81-R94.
4. 4) Nagai K., Ito Y., Yazaki, M., Higuchi, K. and Abe, S.: Development of a Small Six-component Force/torque Sensor Based on the Double-cross Structure, J. Robot. Soc. Jpn., 22 (2004), pp.361-369.
5. 5) Sasoh, A., Sekiya, Y., Sakai, T., Kim, J.-H. and Matsuda, A.: Supersonic Drag Reduction with Repetitive Laser Pulses Through a Blunt Body, AIAA J., 48 (2010), pp.2811-2817.
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