Nonlinear Stochastic Dynamics, Chaos, and Reliability Analysis for a Single Degree of Freedom Model of a Rotor Blade

被引:12
作者
Kumar, Pankaj [1 ]
Narayanan, S. [2 ]
机构
[1] Bharat Heavy Elect Ltd, Gas Turbine Design Dept, Hyderabad 502032, Andhra Pradesh, India
[2] Indian Inst Technol, Dept Mech Engn, Madras 600036, Tamil Nadu, India
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2009年 / 131卷 / 01期
关键词
Fokker-Planck equation; path integral; finite element method; chaos; reliability; nonlinear stochastic dynamics; blade vibration; RANDOM VIBRATION; OSCILLATOR; SYSTEMS;
D O I
10.1115/1.2967720
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In turbomachinery, the analysis of systems subjected to stochastic or periodic excitation becomes highly complex in the presence of nonlinearities. Nonlinear rotor systems exhibit a variety of dynamic behaviors that include periodic, quasiperiodic, chaotic motion, limit cycle, jump phenomena, etc. The transitional probability density function (PDF) for the random response of nonlinear systems under white or colored noise excitation (delta-correlated) is governed by both the foward Fokker-Planck (FP) and backward Kolmogorov equations. This paper presents efficient numerical solution of the stationary and transient form of the forward FP equation corresponding to two state nonlinear systems by standard sequential finite element (FE) method using C(0) shape Junctions and Crank-Nicholson time integration scheme. For computing the reliability of system, the transient FP equation is solved on the safe domain defined by D barriers using the FE method. A new approach for numerical implementation of path integral (PI) method based on non-Gaussian transition PDF and Gauss-Legendre scheme is developed. In this study, PI solution procedure is employed to solve the FP equation numerically to examine some features of chaotic and stochastic responses of nonlinear rotor systems. [DOI: 10.1115/1.2967720]
引用
收藏
页数:8
相关论文
共 26 条
[1]   A non-linear integrated aeroelasticity method for the prediction of turbine forced response with friction dampers [J].
Bréard, C ;
Green, JS ;
Vahdati, M ;
Imregun, M .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2001, 43 (12) :2715-2736
[2]  
CHA D, 1999, ASME, V119, P710
[3]   FIRST-CROSSING PROBABILITIES OF LINEAR OSCILLATOR [J].
CRANDALL, SH .
JOURNAL OF SOUND AND VIBRATION, 1970, 12 (03) :285-+
[5]  
Eugene W., 1965, INT J ENGINEERING SC, V3, P213
[6]   MODEL DEVELOPMENT AND STATISTICAL INVESTIGATION OF TURBINE BLADE MISTUNING [J].
GRIFFIN, JH ;
HOOSAC, TM .
JOURNAL OF VIBRATION ACOUSTICS STRESS AND RELIABILITY IN DESIGN-TRANSACTIONS OF THE ASME, 1984, 106 (02) :204-210
[7]   INVARIANT MEASURE OF A DRIVEN NONLINEAR OSCILLATOR WITH EXTERNAL NOISE [J].
JUNG, P ;
HANGGI, P .
PHYSICAL REVIEW LETTERS, 1990, 65 (27) :3365-3368
[8]  
KUMAR P, 2006, P INDIAN ACAD SCI, V31, P455
[9]  
Kunert A., 1991, VIBRATION ANAL ANAL, VDE-37, P57
[10]   A FINITE-ELEMENT METHOD FOR THE STATISTICS OF NON-LINEAR RANDOM VIBRATION [J].
LANGLEY, RS .
JOURNAL OF SOUND AND VIBRATION, 1985, 101 (01) :41-54