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Устойчивость стержня

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Published on May 8, 2013

Вывод формулы Эйлера для критической нагрузки сжатого прямолинейного упругого стержня при различных условиях закрепления концов. Случай 1: оба конца шарнирые опоры (мю=1). Случай 2: заделка внизу и скользящая заделка вверху.
The derivation of the Euler critical load compressed straight elastic rod at different poles at the ends. Case 1: both ends of the hinge support (mu = 1). Case 2: The seal at the bottom and at the top of the sliding seal.

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