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开发了一套航空发动机叶片槽道激波测试系统。实现了对发动机叶片槽道激波图形绘制的自动化处理,并在某型发动机上进行了成功应用,为航空发动机的相关设计的工作提供了依据。
Developed a set of aeroengine blade channel shock testing system. The automatic processing of the shock wave drawing of the engine blade channel was realized and successfully applied on a certain type of engine, which provided the basis for the related design of aeroengine.