Numerical Simulation of Galileo Probe Entry Flowfield with Radiation and Ablation
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Chofu 182-8522, Japan
2. Tohoku University, Sendai 980-8579, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.10264
Reference37 articles.
1. Galileo Probe Heat Shield Ablation Experiment
2. Analysis of Galileo Probe Heatshield Ablation and Temperature Data
3. Heatshielding problems of planetary entry - A review
4. Injection-induced turbulence in stagnation-point boundary layers
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