升力面方法在冲压空气涡轮性能计算中的应用
APPLICATION OF LIFTING SURFACE METHOD TO RAM AIR TURBINE PERFORMANCE CALCULATION
-
摘要: 应用现代螺旋桨升力面元方法计算冲压空气涡轮的气动性能,叶片采用单层涡模型,尾涡采用与Goldstein假设一致的刚性尾涡,将螺旋马蹄尾涡视为开口涡环以便于编程。对一个模型冲压空气涡轮作数值计算,在小负荷和较大负荷工况下风能利用系数均与实验值符合的较好,涡元控制点的诱导速度和环量分布合理。Abstract: The modern propeller lifting surface method has been applied to calculating the performance of Ram Air Turbine,and a single layer vortex model is adapted to the blade,the wake is modeled to rigid cylinder wake coincided with Goldstein hypothesis.A numerical calculation for a model of Ram Air Turbine shows a good agreement of the coefficient of wind power utilization with its experimental data at both small and large loading.The distributions of induced velocities and circulation are reasonable.
-
Key words:
- Ram air turbines /
- Lifting /
- Surface performance analysis
-
点击查看大图
计量
- 文章访问数: 1738
- HTML浏览量: 108
- PDF量: 554
- 被引次数: 0

下载: