Scaling of Upstream Influence Line Induced by Shock Sweeping Concave Half-Cylinder-Reference-Cited by-同舟云学术

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Scaling of Upstream Influence Line Induced by Shock Sweeping Concave Half-Cylinder

Published:2024-07 Issue:7 Volume:62 Page:2800-2808
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Huang Qi¹,Hong Yuting¹,Li Zhufei¹^ORCID

Affiliation:

1. University of Science and Technology of China, 230027 Hefei, People’s Republic of China

Funder

National Natural Science Foundation of China

Strategic Priority Research Program of Chinese Academy of Sciences

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J063924

Reference36 articles.

1. Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions

2. A review of three-dimensional shock wave–boundary-layer interactions

3. Investigation of shock dynamics in an axisymmetric inlet/isolator with attached boundary layers

4. Dynamics of Three-Dimensional Shock-Wave/Boundary-Layer Interactions

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