HALO3D: An All-Mach Approach to Hypersonic Flows Simulation, Part II
Author:
Affiliation:
1. CFD Laboratory, Department of Mechanical Engineering, McGill University, Montreal, Canada
2. Fluids business unit, Ansys, Inc., Montreal, Canada
3. Fluids business unit, Ansys, Inc., Lebanon, NH, USA
Funder
Mitacs
Natural Sciences and Engineering Research Council of Canada
Lockheed Martin Corporation
Ansys Canada
Publisher
Informa UK Limited
Link
https://www.tandfonline.com/doi/pdf/10.1080/10618562.2024.2306946
Reference85 articles.
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2. Evaluation of Finite-Rate Surface Chemistry Models for Simulation of the Stardust Reentry Capsule
3. Real-Gas Aerothermodynamics Test Facilities;Arnold J. O.;NATO AGARD-AR,1998
4. New Discrete Vibrational Energy Model for the Direct Simulation Monte Carlo Method
5. Nonequilibrium radiation during re-entry at 10 km/s
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