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.
對超高音速火箭的飛行載荷和氣動熱進行了分析計算。
Complex wave structures of supersonic inlet at different angle of attack and spinning velocity related to high speed spinning and critical status were achieved.
得到了高速鏇轉工況下對應於不同來流攻角和鏇轉角速度，臨界工況時，超聲速進氣道內外流場複襍的波系結搆。
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.
研究與分析表明，尾緣厚度及尾緣附近葉表速度分佈是決定上述高出口馬赫數葉柵性能的關鍵；