Planar Measurements of Supersonic Boundary Layers with Curvature Driven Pressure Gradients-Reference-Cited by-同舟云学术

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Planar Measurements of Supersonic Boundary Layers with Curvature Driven Pressure Gradients

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Ekoto Isaac¹,Bowersox Rodney¹,Goss Larry²

Affiliation:

1. Texas A&M University

2. Innovative Scientific Solutions Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1137

Reference39 articles.

1. 1Bradshaw,P.,TheEffectofStreamlineCurvatureonTurbulentFlow,AGARDograph169,1973.

2. 2Schetz,J.A.,BoundaryLayerAnalysis,PrenticeHall,EnglewoodCliffs,N.J.,1993.

3. 3White,F.,ViscousFluidFlow,McGraw-HillHigherEducation,NewYork,2006.

4. 4Schlichting,H.,Boundary-LayerTheory,Springer,NewYork,2003.

Cited by 2 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. Numerical Simulation of Supersonic Turbulent Boundary Layers Subjected to Favorable Pressure Gradients;AIAA SCITECH 2023 Forum;2023-01-19

2. Particle image velocimetry measurements of Mach 3 turbulent boundary layers at low Reynolds numbers;Experiments in Fluids;2018-04-25

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