It was revealed that the ramairturbine performance could be improved by optimizing the blades near the hub region.
数值模拟结果显示在冲压空气涡轮桨叶近轮毂区域需要进一步优化。
2
It was found that the output power of ramairturbine can satisfy the flight refuel needs on conditions that the air speed of wind tunnel is 16% lower than the minimal flight speed of aircraft tanker.