high supersonic velocity

基本解释

The flight loads and dynamic heating of the rocket during flight in a high supersonic velocity are also analyzed and calculated.
对超高音速火箭的飞行载荷和气动热进行了分析计算。
Complex wave structures of supersonic inlet at different angle of attack and spinning velocity related to high speed spinning and critical status were achieved.
得到了高速旋转工况下对应于不同来流攻角和旋转角速度，临界工况时，超声速进气道内外流场复杂的波系结构。
It is shown that the performance of the high supersonic turbine cascade is determined by the thickness of the trailing edge and the velocity distribution on the surface near the trailing edge.
研究与分析表明，尾缘厚度及尾缘附近叶表速度分布是决定上述高出口马赫数叶栅性能的关键；