翼载荷

离散涡线法计算细长翼载荷分布的改进

An improvement in the discrete-vortex method used for calculating the loading distribution on slender delta wings

在同样相对厚度下，变厚度卷弧翼的载荷分布与等厚度卷弧翼的载荷分布相差很小，气动设计时可以不考虑厚度变化的影响。

Results on the measured pressure also indicated that the difference between the load distribution of the equal thickness WAF and that of unequal thickness WAF was small , if the relative thickness is same . Consequently the influence of variation in thickness on the aerodynamic characteristics may be neglected .

远程火箭弹卷弧翼气动载荷工程计算方法

An Engineering Calculating Method of the Aerodynamic Load for Long Range Rocket Projectile Wrap-Around Wings

三翼面飞机前翼和平尾机动载荷优化配置

Maneuver Load Optimal Distribution Between Canard and Horizontal Tail of Three-surface Aircraft

新副翼的形状在总体上保持不变，不过在其末端的横截面积却变小了。三翼面飞机前翼和平尾机动载荷优化配置

The new flap keeps essentially the same profile , but with a reduced cross sectional area at its extremities . Maneuver Load Optimal Distribution Between Canard and Horizontal Tail of Three-surface Aircraft