Immersed boundary conditions for hypersonic flows using ENO-like least-square reconstruction-Reference-Cited by-同舟云学术

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Immersed boundary conditions for hypersonic flows using ENO-like least-square reconstruction

Published:2021-01 Issue: Volume:215 Page:104794
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Bridel-Bertomeu Thibault

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference64 articles.

1. Hypersonic flight simulation-aerodynamics;Potter,1965

2. Simulation of hypersonic scramjet exhaust;Oman,1975

3. Numerical simulation of supersonic and hypersonic turbulent compression corner flows;Hung;AIAA J,1977

4. Numerical simulation of hypersonic viscous fore-and afterbody flowsover capsule-type vehicles at angles of attack;Yamamoto,1985

5. Explosive shocks in air;Kinney,2013

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2. Development of an Immersed Boundary Method for High-Speed Compressible Flows;AIAA SCITECH 2023 Forum;2023-01-19

3. Wall heat flux estimation using the Cartesian cut-cell method;Journal of Fluid Science and Technology;2023

4. Topological Analysis of Ensembles of Hydrodynamic Turbulent Flows An Experimental Study;2022 IEEE 12th Symposium on Large Data Analysis and Visualization (LDAV);2022-10-16

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