Observation of Cross-Flow Instability Mode over a Yawed Cylinder at Mach 2-Reference-Cited by-同舟云学术

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Observation of Cross-Flow Instability Mode over a Yawed Cylinder at Mach 2

Published:2015-01 Issue:1 Volume:53 Page:260-265
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Takagi Shohei¹,Sakaue Shoji²,Hirata Yutaka³,Uemura Takuji³,Takada Kosuke³

Affiliation:

1. Aerospace Plane Research Center, Muroran Institute of Technology, Muroran, Hokkaido 050-8585, Japan

2. Department of Aerospace Engineering, Osaka Prefecture University, Sakai, Osaka 599-8531, Japan

3. Department of Aerospace Engineering, Muroran Institute of Technology, Muroran, Hokkaido 050-8585, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052928

Reference33 articles.

1. Stability of Three-Dimensional Boundary Layers

2. Effect of micron-sized roughness on transition in swept-wing flows

3. Experiments in nonlinear saturation of stationary crossflow vortices in a swept-wing boundary layer

4. Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instability

5. Observation of traveling waves in the three-dimensional boundary layer along a yawed cylinder

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