Flow field of unfold course for a solid rocket engine with extendible nozzle was analyzed by approach numerical solution of the 2-D axis symmetry N-S equation through AF method.

 
  • 文中通過(guò)AF方法求解二維軸對稱(chēng)N-S方程,對采用延伸噴管+的固體火箭發(fā)動(dòng)機級間展開(kāi)過(guò)程地面單試的流場(chǎng)進(jìn)行了數值分析。
今日熱詞
目錄 附錄 查詞歷史
国内精品美女A∨在线播放xuan