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 .
通过已有的例进行验证,结果明靠,以代替以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 .
通过已有的例进行验证,结果明靠,以代替以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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