Akademik Veri Yönetim Sistemi
18th IMAC Conference on Computational Challenges in Structural Dynamics, San-Antonio, Kuzey Mariana Adaları, 7 - 10 Şubat 2000, cilt.4062, ss.1703-1709
Large flexible structures and aerospace structures can be studied by building a model flexible beam with appendage. An appendage can be used as a passive or an active vibration absorber for a structure under sinusoidal and random excitation. In this study, a cantilever beam-tip mass-pendulum system is investigated by using FE method. Dynamical behavior of the model has been investigated under sinusoidal excitation in the neighborhood of autoparametric region Omega=omega(b)=2 omega(p). The autoparametric interaction between the beam and the pendulum (absorber) has been exhibited. Hence, the maximum energy transfer between the beam and the pendulum was observed when the autoparametric resonance condition was satisfied. Detailed analysis has been performed for different mass ratios (pendulum mass/tip mass) and excitation amplitudes. Results show that the pendulum can be used as a passive vibration absorber for flexible structures having low natural frequency.