Wind Tunnel Experiment of Bluff Body Aerodynamic Models Using a New Type of Magnetic Suspension and Balance System

Author:

Kawamura Y.1,Mizota T.2

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

We have measured drag coefficients of a sphere and a circular cylindrical aerodynamic model using a five axes and a six axes control magnetic suspension and balance system (MSBS) developed by us. This MSBS has the characteristics of large aperture relative to the weight, light weight, and small electric power consumption in comparison with the conventional ones. We had good agreements between the measured values of the drag coefficient and the values appearing in the common aerodynamic handbook or textbook. We also succeeded in measuring the aerodynamic influence of a supporting rod of the aerodynamic models making use of the characteristics of the MSBS. Conventionally, the MSBS can be used only in large scale laboratories because the size, weight, and electric power consumption are large. We think that successful measurements of various aerodynamic characteristics using this type of MSBS will stimulate the introduction of it into the wind tunnel experiments in small scale laboratories.

Publisher

ASME International

Subject

Mechanical Engineering

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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