Wind Tunnel Experiment of Bluff Body Aerodynamic Models Using a New Type of Magnetic Suspension and Balance System
Author:
Affiliation:
1. e-mail:
2. Department of Intelligent Mechanical Engineering, Faculty of Engineering, Fukuoka Institute of Technology, 3-30-1, Wajirohigashi, Higashiku Fukuoka, 811-0295, Japan
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/fluidsengineering/article-pdf/doi/10.1115/1.4024793/6189477/fe_135_10_101401.pdf
Reference11 articles.
1. Study on Aerodynamic Force Acting on a Sphere With and Without Boundary Layer Trips Around the Critical Reynolds Number With a Magnetic Suspension and Balance System;Exp. Fluids,2011
2. Kohno, T., Sawada, H., Suenaga, H., and Kunimasu, T., 1995, “NAL 0.6 × 0.6 m MSBS—The Latest Development,” 33rd Aircraft Symposium, Hiroshima, Japan, Nov. 8–11, pp. 345–348.
3. Sawada, H., Kohno, T., and Kunimasu, T., 2000, “Status of MSBS Study at NAL,” NASA/CP-2000-210291, pp. 659–673.
4. Advanced Magnetic Suspension and Balance System Having Characteristics of Light Weight, Electric Power Saving and Fast Response;ASME J. Dyn. Sys., Meas., Control,2012
5. Development of a Simulator of a Magnetic Suspension and Balance System;Int. J. Aero. Space Sci.,2010
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