HALO3D: An All-Mach Approach to Hypersonic Flows Simulation-Reference-Cited by-同舟云学术

HALO3D: An All-Mach Approach to Hypersonic Flows Simulation

Published:2022-03-16 Issue:3 Volume:36 Page:187-206
ISSN:1061-8562
Container-title:International Journal of Computational Fluid Dynamics
language:en
Short-container-title:International Journal of Computational Fluid Dynamics

Author:

Casseau Vincent¹,Zhang Wenbo¹,Mallikarjun Shrutakeerti¹,Habashi Wagdi G.¹,Gao Song²,Karchani Abolfazl³

Affiliation:

1. CFD Laboratory, Department of Mechanical Engineering, McGill University, Montreal, Canada

2. Ansys, Inc., Montreal, Canada

3. Ansys, Inc., Lebanon, NH, USA

Funder

Lockheed Martin

Mitacs

Ansys

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Condensed Matter Physics,Aerospace Engineering,Computational Mechanics

Link

https://www.tandfonline.com/doi/pdf/10.1080/10618562.2022.2094917

Reference77 articles.

1. Finite Element Adaptive Method for Hypersonic Thermochemical Nonequilibrium Flows

2. Fully Transient Conjugate Analysis of Silica-Phenolic Charring Ablation Coupled with Interior Ballistics

3. Evaluation of Finite-Rate Surface Chemistry Models for Simulation of the Stardust Reentry Capsule

4. Hypersonic and High-Temperature Gas Dynamics, Second Edition

5. Barbante, P. F., and T. E. Magin. 2004. “Fundamentals of Hypersonic Flight – Properties of High Temperature Gases.” RTO-AVT Lecture Series RTO-EN-AVT-116.

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