Measurements of Turbulent Flow Structure in Supersonic Curved Wall Boundary Layers-Reference-Cited by-同舟云学术

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Measurements of Turbulent Flow Structure in Supersonic Curved Wall Boundary Layers

Published:2000-01 Issue:1 Volume:16 Page:153-154
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Bowersox R. D. W.¹,Wier R. C.²,Glawe D. D.³,Gogineni S.⁴

Affiliation:

1. University of Alabama, Tuscaloosa, Alabama 35487

2. U.S. Air Force Research Laboratory, Eglin Air Force Base, Florida 32542

3. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

4. Innovative Scientic Solutions, Inc., Dayton, Ohio 45440

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.5546

Reference6 articles.

1. The effect of mean compression or dilatation on the turbulence structure of supersonic boundary layers

2. The Physics of Supersonic Turbulent Boundary Layers

3. Experimental Analysis of the Turbulent Shear Stresses for Distorted Supersonic Boundary Layers

Cited by 12 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. Supersonic Boundary Layers with Periodic Surface Roughness;AIAA Journal;2008-02

2. Mechanically Distorted Supersonic Boundary Layers;25th AIAA Applied Aerodynamics Conference;2007-06-15

3. Response of a Supersonic Turbulent Boundary Layer to Periodic Surface Roughness;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

4. Planar Measurements of Supersonic Boundary Layers with Curvature Driven Pressure Gradients;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

5. Large-scale structure visualization and convection velocity in supersonic blunt-base cylinder wakes;Physics of Fluids;2007-01

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