Investigation of Thermodynamic Non-Equilibrium in Hypersonic Flows Over the Mars Pathfinder Capsule
Author:
Affiliation:
1. University of Campinas
2. Aeronautics and Space Institute (IAE)
Publisher
American Institute of Aeronautics and Astronautics
Reference41 articles.
1. Hypersonic and High-Temperature Gas Dynamics, Second Edition
2. A hybrid numerical scheme for aeroheating computation of hypersonic reentry vehicles
3. A novel flux splitting scheme with robustness and low dissipation for hypersonic heating prediction
4. A grid strategy for predicting the space plane's hypersonic aerodynamic heating loads
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. A Streamline-Upwind Petrov–Galerkin formulation for the analysis of hypersonic flows in thermal non-equilibrium;Computer Methods in Applied Mechanics and Engineering;2022-08
2. Progress in the numerical study on the aerodynamic and thermal characteristics of hypersonic vehicles: High-temperature chemical non-equilibrium effect;SCIENTIA SINICA Physica, Mechanica & Astronomica;2021-09-16
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