大展弦比机翼 high aspect ratio wing
- 试验是在大展弦比机翼颤振模型上进行的。
The tests are conducted on a wing model with large aspect ratio. - 为此建立了大展弦比机翼突风响应的分析方法。
Approaches to calculate the response to continuous and discrete gust for hacw were presented. - 这类飞机普遍具有大展弦比机翼的特点,它的非线性气动弹性问题…
The aeroelastic problems of the UAV are significant due to its high-aspect -ratio wings .
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