The numerical simulation of supersonic inlet internal turbulent flow of solid rocket ramjet assisted range projectiles was performed by 2-order implicit TVD.

 
  • 摘要應用二階隱式TVD格式對固體火箭沖壓發(fā)動(dòng)機增程彈丸超音速進(jìn)氣道內部湍流流場(chǎng)進(jìn)行了數值仿真。
今日熱詞
目錄 附錄 查詞歷史
国内精品美女A∨在线播放xuan