摘要
推导了用于火箭燃气冲击载荷识别的基本关系式。在采取提高识别精度的一系列措施后,取得较理想的模拟载荷识别结果。
In this paper, we deduce the basic relationship for the recognition of rocket exhaust blast loads. After taking a series of steps of improving precision, we obtain the ideal results of the modeling distinguishing of the loads.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
1992年第4期39-44,共6页
Acta Armamentarii
关键词
火箭
燃气流
modal analysis, parameter distinguishing, rocket, exhaust flow
