Finite Element Modeling of Nonequilibrium Fluid–Wall Interaction at High-Mach Regime
Author:
Affiliation:
1. University of Strathclyde, Glasgow, Scotland G1 5HE, United Kingdom
Funder
Natural Sciences and Engineering Research Council of Canada
Lockheed Martin Corporation
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034211
Reference27 articles.
1. AndersonJ. D., Hypersonic and High-Temperature Gas Dynamics, AIAA, Washington, D.C., 1989, pp. 20–23.
2. Predicting Breakdown of the Continuum Equations Under Rarefied Flow Conditions
3. Velocity Slip and Temperature Jump in Hypersonic Aerothermodynamics
4. Predicting continuum breakdown in hypersonic viscous flows
5. Towards Development of a Hybrid DSMC-CFD Method for Simulating Hypersonic Interacting Flows
Cited by 2 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. Hybrid Navier–Stokes–Direct Simulation Monte Carlo Automatic Mesh Optimization for Hypersonics;Journal of Thermophysics and Heat Transfer;2023-10
2. HALO3D: An All-Mach Approach to Hypersonic Flows Simulation;International Journal of Computational Fluid Dynamics;2022-03-16
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