taper ratio

Evaluations are also made on taper equations and volume ratio equations being compared.

另外对所比较的削度方程和材积比方程作了评价。

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The maximum stress in slab surface increases with decreasing the taper ratio of crystallizer, and with increasing the slab width.

随着结晶器锥度减小和连铸坯宽度的增加，连铸坯表层最大应力增加；

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In order to evaluate these two equations, they ase compared respectively with other taper equations and volume ratio equations in use, using data of Chinese fir ( Cunninghamia lanceolata Hook) stands. Results show better effectiveness of these two equations than others.

为了评价这两个方程，利用杉木材料分别与其它已有削度方程和材积比方程作了比较，结果表明这两个方程的效果较好。

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The influence of sweep angle and taper ratio on the characteristics of wingtip stalling is discussed.

讨论了后掠角和尖削比这两个机翼外形参数对翼尖失速特性的影响。

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Taper ratio and optimum value of taper-flat sector thrust bearing with double-side resistive oil edges posterior inclined plane appliance

双封油边斜&平面固定瓦推力轴承的最佳斜面比

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The results showed the voidage ratio of taper spiral packing,θ-ring packing and metal gauze corrugated packing was 0.823:0.947:0.855, and under the same liquid sprayed density, the pressure drop ratio of unit height of packing layer was 0.58:1.10: 0.62.

流体力学性能测试中，锥度螺旋填料、θ环和丝网波纹填料三种填料的空隙率之比为：0.823：0.947：0.855时，在相同喷淋密度下，单位高度填料层压降之比却为：0.58：1.10：0.62。

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The task of the initial sizing is to find the primary parameters of aircraft, including the takeoff wing loading, thrust-to-weight ratio, takeoff weight, wing area, aspect ratio of wing, wing sweep, thickness and taper ratio to match the mission requirements.

其任务是找到能满足飞机性能要求的飞机主要参数。这些参数包括：起飞翼载、推重比、起飞重量、机翼面积、机翼翼载、机翼后掠角、机翼相对厚度和机翼梯形比等。

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