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对７０°三角翼作大幅度仰运动时翼面非定常压力分布和振动鸭翼后面主翼面上非定常压力进行了测量。分析了缩减频率等参数对非定压力分布的影响。
The unsteady pressure distribution of the airfoil and the unsteady pressure on the main airfoil behind the cantilever wing were measured when the 70 ° delta wing was greatly inverted. The effects of parameters such as reduction frequency on the distribution of non-constant pressure were analyzed.