Investigation of Hypersonic Gap Flow of a Reentry Nosecap with Consideration of Fluid Structure Interaction-Reference-Cited by-同舟云学术

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Investigation of Hypersonic Gap Flow of a Reentry Nosecap with Consideration of Fluid Structure Interaction

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Hinderks Michael¹,Radespiel Rolf¹

Affiliation:

1. Braunschweig Technical University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-188

Cited by 8 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. Parametric Study of Cavity Flow;AIAA AVIATION 2022 Forum;2022-06-20

2. Length-to-Depth Ratio Effects on Aerodynamic Surface Quantities of a Hypersonic Gap Flow;AIAA Journal;2018-02

3. On the convergence rate of the Dirichlet–Neumann iteration for unsteady thermal fluid–structure interaction;Computational Mechanics;2017-11-23

4. Effects of width-to-depth ratio on heat transfer coefficient for gap;International Journal of Numerical Methods for Heat & Fluid Flow;2015-05-05

5. Fast solvers for unsteady thermal fluid structure interaction;International Journal for Numerical Methods in Fluids;2015-04-28

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