论文部分内容阅读
在介绍全尺寸飞机进气道/发动机匹配工作流场测试系统的基础上，给出了在发动机前安装飞机前机身后，在地面台架试车时测得的进口压力场数据，计算了进口压力场的畸变指数，分析了流场畸变图谱。
Based on the introduction of the test system of full-size aircraft inlet / engine matching working flow field, the data of inlet pressure field measured at the time of test on the ground platform are given after the front fuselage of the aircraft is installed on the engine, Pressure field distortion index, analysis of the flow field distortion map.