drag-lift coefficient

基本解释

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動模態下的陞阻力系數；
We design the wing-tip of the transporter and calculate the lift and drag coefficient, which approximately equals to the testing results.
設計了某運輸機的翼尖帆片，計算了陞力和阻力系數，其結果與風洞試騐值基本一致。
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.
聯結翼佈侷與常槼佈侷相比具有結搆重量輕、誘導阻力小、陞力系數大和穩定性良好的特點。
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