This paper discusses the development of an efficient algorithm which calculates the individual blade response of a bladed turbine disk, the subsequent statistical investigation to establish mistuning dependencies, and procedures which reduce the increase in blade amplitudes caused by mistuning.

Issue Section:
Vibrations of Bladed-Disk Assemblies
Topics:
Algorithms, Blades, Disks, Model development, Turbine blades, Turbines
This content is only available via PDF.
Copyright © 1984
 by ASME
You do not currently have access to this content.