This paper has supplied a valuable analytical method to study aeroelastic problems produced by shock wave oscillation.
本文为激波振荡导致的气动弹性问题提供了一种有价值的理论方法。
2
One of the more severe fluctuating pressure environments encountered in supersonic or hypersonic flows is the shock wave oscillation driven by interaction of a shock wave with boundary layer.
在超声速或高超声速绕流中，一种很严重的脉动压力环境是由激波边界层相互作用引起的激波振荡。
3
This scheme is also used to simulate a two-dimensional viscous flow. Calculation results confirm its high accuracy and high resolutions, good ability in capture shock and no oscillation.