两种有翼飞行器高超声速动态气动特性的对比实验研究

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Publication date
1 January 2001
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Abstract

采用模型自由飞技术在脉冲型高超声速风洞中测量了两种类航天飞机外形模型的俯仰阻尼导数。两种模型具有十分接近的外形特征尺寸和投影面积，但机身和机翼的剖面则彼此各不相同

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