Numerical Simulation of Weakly Ionized Dynamic Plasma for Reentry Vehicles
Author:
Affiliation:
1. Zhejiang University, 310027 Hangzhou, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33525
Reference36 articles.
1. Governing Equations for Weakly Ionized Plasma Flowfields of Aerospace Vehicles
2. Non-equilibrium flowfield of RAM-C II probe
3. Electromagnetic Reduction of Plasma Density During Atmospheric Reentry and Hypersonic Flights
4. Introduction of the PIRATE Program for Parametric Reentry Vehicle Plasma Effects Studies
5. Calculation of the Effect on the Reflection of the Plane Electromagnetic Wave for Non-Magnetized Plasma with Different Electron Density Distributions
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