wind tunnel test data base 风洞试验数据库
This paper briefly presents a method of uncertainty analysis for wind tunnel test data.
本文简要介绍了风洞数据不确定度分析方法。
In this paper, the initial stage in application of fuzzy logic to aircraft high-Angle-of attack aerodynamics using wind tunnel test data is outlined.
本文概述最初阶段利用风洞试验数据应用模糊逻辑研究飞机大攻角空气动力学的情况。
Through analyzing the methods and combination of the low speed wind tunnel test data, the position of the separation point can be detected accurately.
通过对试验结果进行数据处理，验证了该判定方法对分离点位置判定的正确性和有效性。
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