这就是“土星”飞行器安定面尺寸选择的主要依据。
This was the primary reason for selecting the fin size for the Saturn Vehicle.
为验证该算法，给出了一个飞机水平安定面翼肋设计实例。
To test this algorithm, one design example, one rib of an aircraft wing, is given.
为验证该算法，给出了一个飞机水平安定面翼肋设计实例。
To test this algorithm, one design example, one rib of an aircraft wing, is given.
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