Experimental investigation of transonic and supersonic flow over a sphere for Reynolds numbers of 103–105 by free-flight tests with schlieren visualization-Reference-Cited by-同舟云学术

Experimental investigation of transonic and supersonic flow over a sphere for Reynolds numbers of 103–105 by free-flight tests with schlieren visualization

Published:2019-09-27 Issue:2 Volume:30 Page:139-151
ISSN:0938-1287
Container-title:Shock Waves
language:en
Short-container-title:Shock Waves

Author:

Nagata T.^ORCID,Noguchi A.,Nonomura T.^ORCID,Ohtani K.^ORCID,Asai K.

Funder

Japan Society for the Promotion of Science

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/s00193-019-00924-0.pdf

Reference24 articles.

1. Taneda, S.: Experimental investigation of the wake behind a sphere at low Reynolds numbers. J. Phys. Soc. Jpn 11(11), 1104–1108 (1956). https://doi.org/10.1143/JPSJ.11.1104

2. Taneda, S.: Visual observations of the flow past a sphere at Reynolds numbers between 104 and 106. J. Fluid Mech. 85(1), 187–192 (1978). https://doi.org/10.1017/S0022112078000580

3. Sakamoto, H., Haniu, H.: A study on vortex shedding from spheres in a uniform flow. ASME Trans. J. Fluids Eng. 112, 386–392 (1990). https://doi.org/10.1115/1.2909415

4. Magarvey, R.H., Bishop, R.L.: Transition ranges for three-dimensional wakes. Can. J. Phys. 39(10), 1418–1422 (1961). https://doi.org/10.1139/p61-169

5. Johnson, T.A., Patel, V.C.: Flow past a sphere up to a Reynolds number of 300. J. Fluid Mech. 378(10), 19–70 (1999). https://doi.org/10.1017/S0022112098003206

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