本方法可用于水翼及水下安定翼和各种舵的水动力计算。
This method can be used for the hydrodynamic computation of the varied hydrofoils and stabilizing fins.
尾平翼特征是顶端有一个上端后掠的垂直安定翼和锥形尾垂翼具有一个钝形顶端。
The tail flats feature swept-back tips forward of the swept-back and tapered fin with a blunt tip.
这架飞机拥有由玻璃纤维和碳纤维制成的双体机身，由前部的鸭翼、中部的机翼和尾部的水平安定面连接在一起。
The vehicle sports twin-fuselages made of fiberglass and carbon fiber which are connected by a canard in the front, an airfoil in the middle and a horizontal stabilizer.
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