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.
根据实际问题的物理模型，并通过对机翼颤振模型设计原理的分析，建立了优化设计的数学模型；
The math model, based on real physical one, was modeled according the essential theory and design course of the flutter wing model designing.
在此基础上建立了完整的机翼颤振模型工程优化设计方法，使该方法能够应用在模型设计的很多方面，为工程设计提供了一种有效的手段。
An optimization method of flutter wing model was developed and was used in many aspects of model designing, providing an efficient design method in engineering.
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