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没有一个合适的端板尺寸将会阻止翼根绕流。
得出的结论对于类似的地效飞行器或轻型飞机翼根连接设计具有一定参考价值。
And the conclusions are valuable for wing root joint designs such as those of ground effect aircraft or light airplane.
以复合材料机翼翼根后梁下缘条对接试件为研究对象，通过有限元手段分析其失效机理和破坏过程，并对极限强度进行预测。
Abstract :Failure process of a primary load-bearing composite joint in wing root was analyzed by finite element methods, and the ultimate strength of the joint was predicted.
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