Heat Transfer to Separated and Reattached Subsonic Turbulent Flows Obtained Downstream of a Surface Step-Reference-Cited by-同舟云学术

Heat Transfer to Separated and Reattached Subsonic Turbulent Flows Obtained Downstream of a Surface Step

Published:1959-12 Issue:12 Volume:26 Page:809-814
ISSN:1936-9999
Container-title:Journal of the Aerospace Sciences
language:en
Short-container-title:Journal of the Aerospace Sciences

Author:

SEBAN R. A.¹,EMERY A.¹,LEVY A.¹

Affiliation:

1. University of California at Berkeley,

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.8324

Reference10 articles.

1. Experiments on two-dimensional flow over a normal wall

2. Hsu, H., Characteristics of Mean Flow and Turbulence at an Abrupt Two-Dimensional Expansion, Ph.D. dissertation,State University of Iowa, 1950.

3. Seban, R. A., Heat Transfer and Flow With Separated and Reattached Boundary Layers as Produced by Surface Irregularities, WADC Report TR-56-217, 1956.

4. Emery, A., Heat Transfer Downstream of a Step in a Plate, M.S. thesis,University of Californiaat Berkeley,January, 1958.

5. Velocity and Temperature Profiles in Turbulent Boundary Layers With Tangential Injection

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