supersonic sharp cone boundary layer 超音速尖锥边界层
This means although the normal velocity is not small in the basic flow of the supersonic compressible sharp cone boundary layer, for small semi-angle, LST can still be used.2.
表明虽然零攻角超音速尖锥边界层的基本流有一定的锥面法向速度,当半锥角较小时,平行流假设下的线性理论仍成立。
参考来源 - 零攻角尖锥边界层中二维扰动演化特征的数值研究·2,447,543篇论文数据,部分数据来源于NoteExpress
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