Mechanism of sidewall effect studied with oil flow visualization-Reference-Cited by-同舟云学术

Mechanism of sidewall effect studied with oil flow visualization

Published:1989-12 Issue:12 Volume:27 Page:1828-1830
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Su Yaoxi¹

Affiliation:

1. Northwestern Polytechnical University, Xian, China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.10344

Reference6 articles.

1. Preston, J. H. "The Interference on a Wing Spanning a Closed Tunnel, Arising from the Boundary Layers on the Sidewalls, With Special Refererence to the Design of Two-Dimensional Tunnels,0Aeronautical Research Council R&M 1924, March 1944.

3. Recent sidewall boundary-layer investigations with suction in the Langley 0.3-m Transonic Cryogenic Tunnel

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