The ice accretion geometric characteristics have complex effects on airfoil aerodynamic coefficients.
积冰几何形状对翼型气动系数的影响是复杂的。
The buffet onset boundary is defined as the begin point of increased suddenly fluctuating value of aerodynamic coefficients.
根据气动力系数的脉动量急剧上升的起始点确定抖振起始边界。
The prediction of aerodynamic coefficients for projectile configurations is essential in assessing the performance of new designs.
该配置的弹丸气动系数的预测是必不可少的评估新设计的性能。
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