Flow features of swept shock/turbulent boundary-layer interaction due to a gap beneath a sharp fin-Reference-Cited by-同舟云学术

Flow features of swept shock/turbulent boundary-layer interaction due to a gap beneath a sharp fin

Published:2022-11 Issue: Volume:130 Page:107934
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Otten Dustin L.^ORCID,Lu Frank K.^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference56 articles.

1. Fifty years of shock-wave/boundary-layer interaction research: what next?;Dolling;AIAA J.,2001

2. Experimental studies of quasi-two-dimensional and three-dimensional viscous interaction regions induced by skewed-shock and swept-shock boundary layer interaction;Holden,1984

3. Turbulent shock-wave/boundary-layer interactions;Délery,1986

4. Shock Wave-Boundary-Layer Interactions;Babinsky,2011

5. Supersonic and hypersonic shock/boundary-layer interaction database;Settles;AIAA J.,1994

Cited by 5 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. Scaling of Upstream Influence Line Induced by Shock Sweeping Concave Half-Cylinder;AIAA Journal;2024-07

2. A review of three-dimensional shock wave–boundary-layer interactions;Progress in Aerospace Sciences;2023-11

3. Experimental and numerical investigation of shock wave/boundary layer interactions induced by curved back-swept compression ramp;Aerospace Science and Technology;2023-11

4. Study of Shock/Boundary-Layer Interactions Generated by a Sharp Fin Mounted above a Body of Revolution;25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2023-05-27

5. Flow on Leeward Side of a Sharp Fin Undergoing Swept Shock/Turbulent Boundary-Layer Interaction;AIAA SCITECH 2023 Forum;2023-01-19