2D steady wake predictions for airfoil cascades with beveled trailing edges-Reference-Cited by-同舟云学术

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2D steady wake predictions for airfoil cascades with beveled trailing edges

Published:1997-01-06 Issue: Volume: Page:
ISSN:
Container-title:35th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Knight Charles¹,Peltier Leonard¹,Knight Charles¹,Peltier Leonard¹

Affiliation:

1. Pennsylvania State Univ., University Park

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-77

Reference19 articles.

1. Lecture Notes in Engineering;Blake W.K.,1989

2. An Experimental Investigation of the Flow Through an Axial-Flow Pump

3. W.C. Zierke, W.A. Straka, and P.D. Taylor, "The High Reynolds Number Flow through an Axial-Flow Pump," Applied Research Laboratory Technical Report No. TR 93-12, Penn State University, November 1993.

4. Unsteady viscous simulation for beveled trailing edge flow fields

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Selection of the Simulation Domain for Turbulent Flow Around an Airfoil;Fluids Engineering;2006-01-01

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