Influence of Boundary-Layer Thickness on Base Pressure and Vortex Shedding Frequency-Reference-Cited by-同舟云学术

Influence of Boundary-Layer Thickness on Base Pressure and Vortex Shedding Frequency

Published:2001-04 Issue:4 Volume:39 Page:754-756
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Rowe A.¹,Fry A. L. A.¹,Motallebi F.¹

Affiliation:

1. University of London, London, England E1 4NS, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1377

Reference12 articles.

1. The Base Pressure Problem in Transonic Turbine Cascades

2. Xu, L. “The Base Pressure and Trailing Edge Loss of Transonic Blades,” Ph.D. Dissertation, Dept. of Engineering,Univ. of Cambridge, Cambridge, England, U.K.Jan. 1985.

3. The Influence of Boundary Layer State on Vortex Shedding From Flat Plates and Turbine Cascades

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