Numerical simulation of transpiration cooling on stagnation line in thermochemical non-equilibrium
Sharp leading edges offer drag and maneuverability advantages for hypersonic applications such as powered flight and some gliding trajectories. The reduction in standoff distance resulting from the adoption of sharp edges, however, results in increased surface convective heating that needs to be man...
| Những tác giả chính: | , , , , |
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| Định dạng: | Conference item |
| Ngôn ngữ: | English |
| Được phát hành: |
Aerospace Research Central
2024
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