Abstract
A two-step method is presented for the determination of reliable approximations of the probability density function of the forced response of a randomly mistuned bladed disk. Under the assumption of linearity, an integral representation of the probability density function of the blade amplitude is first derived. Then, deterministic perturbation techniques are employed to produce simple approximations of this function. The adequacy of the method is demonstrated by comparing several approximate solutions with simulation results.
Original language | English (US) |
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Pages (from-to) | 771-780 |
Number of pages | 10 |
Journal | Journal of Turbomachinery |
Volume | 115 |
Issue number | 4 |
DOIs | |
State | Published - Oct 1993 |
ASJC Scopus subject areas
- Mechanical Engineering