摘要
主要阐述了弹丸头部喷流风洞实验中的实验方法、气动力干扰影响及预测方法。介绍了气动力测量、压力测量、底阻测量的关键技术及解决途径。
This paper introduces a wind tunnel experiment technique of side-back jet,aerodynamic interactions and predict method. The key technique of aerodynamic measure, pressure measure and base drag force measure is also discussed.
出处
《航空计测技术》
2004年第5期23-25,31,共4页
Aviation Metrology & Measurement Technology
