Friction dampers are widely used to improve the performance of rotating blades. This paper is concerned with the steady state response and stability analysis of rotating composite plates in the presence of non linear friction damping. Direct Integration Method (DIM) and Harmonic Balance Method (HBM) are used to determine the steady state response due to periodic lateral external forces. In addition, an alternate procedure, Hybrid Method (HM) is proposed for this analysis to substantiate the results from DIM and HBM. The analysis shows that the steady state response is a function of friction damping magnitude as well as its location besides the excitation frequency and the rotational speed. A stability analysis of the composite blades is also made by including periodic in-plane excitation using Floquet-Lyapunov theory.
|頁（從 - 到）||10|
|期刊||American Society of Mechanical Engineers (Paper)|
|出版狀態||Published - 1996 1月 1|
|事件||Proceedings of the 1996 International Gas Turbine and Aeroengine Congress & Exhibition - Burmingham, UK|
持續時間: 1996 6月 10 → 1996 6月 13
All Science Journal Classification (ASJC) codes