The spanwise distributionof lift for minimum induced drag of wings having a given lift and a given bendingmoment.
分布展升降机最低诱导阻力的机翼有鉴于一部升降机和弯曲某一特定时刻。
2
The counterweight is installed on the crankshaft for reducing the bendingmoment on it, but it will influence the magnitude and distributionof the main bearing load.
曲轴上平衡重的安装减小了曲轴所受的弯矩,但也影响了主轴承载荷的大小和分布。
3
Starting with the principle ofmomentdistribution method, the paper applies sequence theory to derive the formula of rod-end bendingmoment.