lift drag coefficient

基本解釋

The lift and drag coefficient of flapping-wing MAV in different motion modes are calculated.
計算了撲翼微飛行器在不同運(yùn)動模態(tài)下的升阻力系數(shù)；
Such parameters of flow characteristics are investigated as lift and drag coefficient and vortex shedding frequencies.
計算了圓柱的升阻力系數(shù)、尾渦脫落頻率等描述繞流問題的主要參量。
We design the wing-tip of the transporter and calculate the lift and drag coefficient, which approximately equals to the testing results.
設(shè)計了某運(yùn)輸機(jī)的翼尖帆片，計算了升力和阻力系數(shù)，其結(jié)果與風(fēng)洞試驗(yàn)值基本一致。