• One of the features of a forced oscillation is the energy in the oscillation.

    受迫振动的特点之一是振动的能量。

    youdao

  • Some problems of the study on forced oscillation pattern of A2B model are discussed.

    讨论了A2B模型的受迫振动模式研究中的一些问题。

    youdao

  • Several forced oscillation criteria are established for such systems subject to two different boundary conditions.

    建立了这类系统在两类不同边界条件下强迫振动的若干判别准则。

    youdao

  • Based on the data from forced oscillation tests of rigid cylindrical sections, many empirical tools were developed.

    近年来出现的若干经验模型基于圆柱体受迫振荡实验数据。

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  • The resonant solution on forced oscillation of A2B model is given and the modes of vibration on resonant frequency are discussed.

    给出了A2B模型受迫振动的两个共振解,讨论了共振频率下的振动模式。

    youdao

  • In this paper, we study the forced oscillation and the strong oscillation of systems of impulsive neutral parabolic differential equations with several delays.

    本文研究了一类脉冲中立型时滞抛物方程解的振动性及强振动性,获得了此类脉冲中立型时滞抛物方程解振动和强振动的代数判据。

    youdao

  • The bifurcation and chaotic process of two-dimensional parallel wall shear flows are described by the forced oscillation equation containing a square nonlinear term.

    二维平行壁面剪切流动进入混沌的现象可用含二次非线性项的强迫振动方程来描述。

    youdao

  • The test results show that the scale, intensity, pairing and merging of the vortices depend, to a large extent, on the forced oscillation frequencies of the spoiler.

    拢流片振动频率,对分离涡的尺度、强弱、成对、合并过程有重要影响。

    youdao

  • Variations of propylene conversion, acrolein selectivity and yield were investigated experimentally by various forced oscillation patterns and compared with the results of steady-state operation.

    实验考察了在不同强制振荡周期与振幅下的丙烯转化率和丙烯醛选择性及收率的变化,并与稳态反应条件下的结果作了比较。

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  • It is shown the nonlinear aerodynamic model given by the article can accurately calculate aerodynamic responses of aircraft models in large amplitude forced oscillation tests at high angles of attack.

    实际计算结果表明该非线性气动力模型能够较为精确地计算飞机模型大幅值迎角简谐振动产生的气动力响应。

    youdao

  • It is shown the nonlinear aerodynamic model given by the article can accurately calculate aerodynamic responses of aircraft models in large amplitude forced oscillation tests at high angles of attack.

    实际计算结果表明该非线性气动力模型能够较为精确地计算飞机模型大幅值迎角简谐振动产生的气动力响应。

    youdao

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