The result was shown that the program runs quickly and in reliability ,It can replace the nomograph method and use easily for predicating sonic fatigue life of aircraft skin-panel structure .
通过已有的算
进行验证，结果表明计算迅速可靠，可
代替列线图为主要手段的求解方法，广泛的应用于工程领域。
The result was shown that the program runs quickly and in reliability ,It can replace the nomograph method and use easily for predicating sonic fatigue life of aircraft skin-panel structure .
通过已有的算进行验证，结果表明计算迅速可靠，可代替列线图为主要手段的求解方法，广泛的应用于工程领域。
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