论文部分内容阅读
本文应用应验数据和计算流体力学(CFD)方法对飞机的NACA辅助进气口性能进行了仿真,分析了进气口在小流量工况下的性能。
In this paper, the performance of the NACA auxiliary air intake of the aircraft is simulated with the experimental data and computational fluid dynamics (CFD) method. The performance of the air intake at low flow rate is analyzed.