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....
| Автори: | , , |
|---|---|
| Формат: | Journal article |
| Опубліковано: |
American Institute of Aeronautics and Astronautics
2019
|