数值算例表明该方法是求解带操纵面偏转的机翼绕流的有效方法。
Numerical results show that the present method is effective for solving the flow around a wing with control surface deflection.
振动圆柱绕流的一个重要特征就是出现锁定现象。
本文对治导建筑物绕流的研究现状作了简要述评。
Review of flow near training structure is presented in this paper.
应用推荐