摘要
由于试验的风洞不同,试验模型不同,测压试验数据积分带来的误差等原因,导致了测压试验数据积分结果与部件测力试验结果不一致,这样的两套数据难以用于型号设计。为此,笔者采用了一种以部件测力试验为基础,将测压试验数据积分结果及其分布协调处理到与部件测力试验结果一致的方法,并用于型号的设计研制中。
As a result of the difference between wind tunnels, the models and the test errors results integrated from the pressure distribution data are different from the results of parts force measurement, such data are difficult to be applied to the model design. Therefore, the author has adopted a method which makes the results from pressure distribution data be assorted with the data from the parts force measurement and put into use in the model design.
出处
《流体力学实验与测量》
CSCD
北大核心
2003年第3期71-75,共5页
Experiments and Measurements in Fluid Mechanics
关键词
飞机
测压试验
数据处理
法向力
压心
测力试验
pressure distribution measurement
parts force measurement
normal force
the center of pressure