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本文研究如何应用矩阵初参数法求解后掠飞机全机自由自由振动问题,指出了几种解法。对其中一种解法导出全部矩阵公式,设计出电子计算机的程序。附有计算例题, 与精确解及试验数据作了比较。悬臂机翼及导弹弹身的振动问题只是本问题的特例。
This paper studies how to solve the problem of free-standing free-vibration of full-scale aircraft with swept aircraft by using the matrix parameter method. Several solutions are pointed out. On one of the solutions to derive all the matrix formula, the design of the computer program. With calculation example, compared with the exact solution and test data. The vibration problem of cantilever wings and missile shells is only a special case of this problem.