The leverage on the performance of aerospace plane from boundary layer transition is presented in outline.

本文概述了边界层转捩对空天飞机性能的影响。

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The mechanism of the effect is that the transition induced normal force arise when the boundary layer transition appear on the slender cone.

影响的基本机理是锥面的边界层在转捩时形成了负方向的诱导法向力。

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In wind tunnel test, tripping wires or a local surface roughness are often applied to fixing the boundary layer transition on airfoils or wings.

在翼型或机翼的风洞试验中，常用绊线或局部表面粗糙度来固定边界层转捩。

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