unsteady aerodynamic loading 非定常气动载荷
aerodynamic loading computation 空气动力学计算
aerodynamic loading on airfoil 机翼空气动力载荷
non-steady aerodynamic loading 非定常气动载荷
The effects of turbomachinery blade bow and sweep on aerodynamic loading distribution of the blade are investigated.
研究叶轮机叶片的弯扭及掠形等因素对叶片气动负荷分布的影响。
Based on the generalized dynamic inflow theory and classic non-steady aerodynamic loading theory, a real time model is obtained by establishing wake distortion and decay.
在广义动态入流理论的基础上，基于经典非定常气动载荷理论，建立了尾迹畸变和尾迹耗散的实时分析模型。
Thus, the aerodynamic performance of stage is im-proved obviously, the profile loss decreases through using the "after loading" blade.
优化的“后部加载”叶型明显提高了气动性能，降低了叶型能量损失。
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