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二元机翼非定常压强分布测量初步研究
引用本文:林维勋. 二元机翼非定常压强分布测量初步研究[J]. 空气动力学学报, 1988, 0(2)
作者姓名:林维勋
作者单位:中国空气动力研究与发展中心
摘    要:本文研究了襟翼作简谐振动的二元机翼模型非定常压强分布测量试验技术。介绍了研究模型、设备和方法。给出了典型的研究结果。这些结果与国外文献给出的数据规律一致,说明了本项研究采用的技术和数据处理方法是可行的。

关 键 词:非定常压力测量  二元机翼  襟翼

A PRELIMINARY INVESTIGASION OF UNSTEADY PRESSURE MEASUREMENT ON A TWO-DIMENSIONAL WING MODEL
Lin Weixun. A PRELIMINARY INVESTIGASION OF UNSTEADY PRESSURE MEASUREMENT ON A TWO-DIMENSIONAL WING MODEL[J]. Acta Aerodynamica Sinica, 1988, 0(2)
Authors:Lin Weixun
Affiliation:China Aerodynamics Research and Development Center
Abstract:A preliminary experimental investigation of unsteady pressure measurement technique is presented on two-dimensional wing model with flap oscillating in pitch.The model,equipment and test method are described and some typical results are given.The regularity of the data agrees with the results given in reference [1],indicating the technique and data processing methods used are feasible.
Keywords:unsteady pressure two-dimensional wing  flaps.
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