Swept-Wing Boundary-Layer Transition and Turbulent Flow Physics from Multipoint Measurements-Reference-Cited by-同舟云学术

Swept-Wing Boundary-Layer Transition and Turbulent Flow Physics from Multipoint Measurements

Published:2014-02 Issue:2 Volume:52 Page:338-347
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Glauser Mark N.¹,Saric William S.²,Chapman Keith L.³,Reibert Mark S.⁴

Affiliation:

1. Department of Mechanical and Aerospace Engineering, Syracuse University, Syracuse, New York 13244

2. Department of Aerospace Engineering, Texas A&M University, College Station, Texas 77843-3141

3. Department of Mechanical and Aeronautical Engineering, Clarkson University, Potsdam, New York 13699

4. Department of Mechanical and Aerospace Engineering, Arizona State University, Phoenix, Arizona 85004

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052479

Reference39 articles.

1. Application of multi-point correlation techniques to aerodynamic flows

2. Boundary-layer transition detection and structure identification through surface shear-stress measurements

3. Stability of Three-Dimensional Boundary Layers

4. DagenhartJ. R. “Crossflow Stability and Transition Experiments in a Swept-Wing Flow,” Ph.D. Dissertation, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, 1992;

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