摘要
本文首先介绍飞机载荷测试微机处理系统的组成,然后对采集的应变量数据建立线性化数学模型,并且介绍了计算应力值的公式,最后给出了测试程序的流程图。
In this paper, at first, it introduced component of microcomputer system in the test of putting pressure on the plane, then infer a math model of the linearization on reacting quantization data, and introduced the formalus about calculating neacting force value, and design software flow chart is given at last.
出处
《辽宁大学学报(自然科学版)》
CAS
1996年第1期66-71,共6页
Journal of Liaoning University:Natural Sciences Edition