...力矩（Aerodynamic Rolling Moment） 的表达式为 bSVCbQSCLwlwlA221 (2.33) 气动俯仰力矩（Aerodynamic Pitching Moment） 的表达式为 AwmlwmAcSVCbQSCM221 (2.34) 气动偏航力矩（Aerodynamic Yawing Moment） 的表达式为 bSVCbQSCNwnwnA221...
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考虑了不同飞行攻角、不同燃料流率下气动参数，包括升力系数、阻力系数和俯仰力矩系数的变化规律。
The change rules of aerodynamic parameters including lift coefficient, drag coefficient and pitch moment coefficient have been analyzed when Angle of attack and fuel flow rate is changed.
基于附着流状态下的旋翼非定常翼型气动模型，给出了计算该状态下的翼型非定常升力、阻力和俯仰力矩的数值计算方法。
A numerical method is given to calculate the unsteady lift, pitching moment and drag acting on an airfoil of rotors under attached-flow conditions in a compressible flow.
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