The problem of unsteady separated flow of rapidly pitching airfoil with oscillatingmotion is computationally studied.
对带振荡的快速上仰翼型的非定常分离流问题进行了计算研究。
2
To analyze the cause of design error on Oscillating follower Cylinder Cam Mechanism, building the mathematics model, and affording the equation to conform to actual motion rule.
分析了摆动从动件圆柱凸轮机构误差产生原因，建立了数学模型，并给出其实际运动规律的方程。
3
The results show that unsteady aerodynamic characteristics of a delta wing oscillating in large amplitude pitching roll motion are more complicated than in pitching motion or in roll motion.