Experimental Study on Vortex Shedding and Sound Radiation from a Rectangular Cylinder at Low Mach Numbers
Author:
Affiliation:
1. Department of Aerospace Engineering, Tokyo Metropolitan University
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/59/5/59_T-15-6/_pdf
Reference27 articles.
1. 1) Lighthill, M. J.: On Sound Generated Aerodynamically I: General Theory, Proc. R. Soc. London A, 211 (1952), pp. 564–587.
2. 2) Curle, N.: The Influence of Solid Boundaries upon Aerodynamic Sound, Proc. R. Soc. London A, 231 (1955), pp. 505–514.
3. 3) Phillips, O. M.: The Intensity of Aeolian Tones, J. Fluid Mech, 1 (1956), pp. 607–624.
4. 4) Kovasznay, L. S. G.: Hot-wire Investigation of the Wake behind Cylinders at Low Reynolds Numbers, Proc. R. Soc. London A, 198 (1949), pp. 174–190.
5. 5) Keefe, R. T.: Investigation of the Fluctuating Forces Acting on a Stationary Circular Cylinder in a Subsonic Stream and of the Associated Sound Field, J. Acoustical Soc. Am., 34 (1962), pp. 1711–1714.
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