V211
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.
谭献忠 陈少松 丁则胜 徐琴.弹丸头部喷流的风洞实验测试技术[J].计测技术,2004,(5):23~25,31:[doi].
