Laminar boundary layer separation at a fin-body junction in a hypersonic flow-Reference-Cited by-同舟云学术

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Laminar boundary layer separation at a fin-body junction in a hypersonic flow

Published:2001-03 Issue:1 Volume:11 Page:31-42
ISSN:0938-1287
Container-title:Shock Waves
language:en
Short-container-title:Shock Waves

Author:

Houwing A.F.P.,Smith D.R.,Fox J.S.,Danehy P.M.,Mudford N.R.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/PL00004055.pdf

Cited by 32 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. Fluid-Structure Interactions of a Hemispherically Rounded Blunt Fin over a Compliant Panel in Mach 2 Flow;AIAA AVIATION 2023 Forum;2023-06-08

2. Dual Numerical Solution for 3D Supersonic Laminar Flow Past a Blunt-Fin Junction: Change in Temperature Ratio as a Method of Flow Control;Fluids;2023-05-11

3. Molecular Tagging Velocimetry in Gases;Optical Diagnostics for Reacting and Non-Reacting Flows: Theory and Practice;2023-01

4. Heat Flux on a Hypersonic Cone with a Highly Swept Fin;Journal of Spacecraft and Rockets;2022-11

5. RANS-based numerical simulation of shock wave/turbulent boundary layer interaction induced by a blunted fin normal to a flat plate;Computers & Fluids;2022-10

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