Tool for rapid transient transpiration cooled re-entry simulation
This Paper presents a numerical model intended for a system study of transpiration-cooled thermal protection systems. The code PIRATE enables rapid transient calculations for thermal protection systems of hypersonic flight vehicles. In the code, semi-empirical aerodynamic correlations are employed....
| 主要な著者: | , , |
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| フォーマット: | Journal article |
| 出版事項: |
American Institute of Aeronautics and Astronautics
2019
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