Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction using Laser Diagnostics-Reference-Cited by-同舟云学术

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Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction using Laser Diagnostics

Published:2016-06-10 Issue: Volume: Page:
ISSN:
Container-title:32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Combs Christopher S.¹,Lash E. Lara¹,Schmisseur John D.¹

Affiliation:

1. University of Tennessee, Tullahoma

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4321

Reference28 articles.

1. A review of aerothermal problems associated with hypersonic flight

2. Progress in shock wave/boundary layer interactions

3. Shock wave boundary layer interaction

4. Interactions between shock waves and turbulent boundary layers

Cited by 26 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. Flow Control of Hypersonic Shock-Wave/Boundary-Layer Interactions Using Phononic Metamaterials;AIAA SCITECH 2024 Forum;2024-01-04

2. Camera-Based Detection of Cylindrical Lens Based Focused Laser Differential Interferometry;AIAA SCITECH 2024 Forum;2024-01-04

3. Upstream Influence in Shock Wave/Transitional Boundary Layer Interactions at Mach 1.8;AIAA Journal;2021-12

4. Exploration of Upstream Influence and the Role of Shock Generator Geometry in Shock Wave/Transitional Boundary Layer Interactions at Mach 1.8 Edge Conditions;AIAA AVIATION 2020 FORUM;2020-06-08

5. Unsteady Analysis of Shock-Wave/Boundary-Layer Interaction Experiments at Mach 4.2;AIAA Journal;2019-11

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