drag-lift coefficient

基本解释

The lift and drag coefficient of flapping-wing MAV in different motion modes are calculated.
计算了扑翼微飞行器在不同运动模态下的升阻力系数；
We design the wing-tip of the transporter and calculate the lift and drag coefficient, which approximately equals to the testing results.
设计了某运输机的翼尖帆片，计算了升力和阻力系数，其结果与风洞试验值基本一致。
The joined-wing configuration, as compared with the normal configuration, is characterized by low structural weight, small induced drag, big lift coefficient and good stability.
联结翼布局与常规布局相比具有结构重量轻、诱导阻力小、升力系数大和稳定性良好的特点。
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