Regenerativecooling technology is one of the key technologies to thermally protect scramjet chamber.
再生冷却技术是超燃冲压发动机燃烧室热防护的关键技术。
2
The influences of porosity on the local blowing ratio, wall temperature and boundary layer thickness were compared with the effects with regenerativecooling.
对比再生冷却分析了不同注入率对壁面温度、冷却效率以及边界层厚度的影响；
3
Then using this method, influence of gas wall material, gas wall thickness and flow rate of coolant on regenerativecooling of thrust chamber was investigated. The results were satisfactory.