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RESEARCH PAPERS

A Study of the Modal Truncation Error in the Component Mode Analysis of a Dual-Rotor System

[+] Author and Article Information
D. F. Li, E. J. Gunter

Mechanical and Aerospace Engineering Department, University of Virginia, Charlottesville, Va. 22901

J. Eng. Power 104(3), 525-532 (Jul 01, 1982) (8 pages) doi:10.1115/1.3227311 History: Received December 15, 1980; Online September 28, 2009

Abstract

In the component mode synthesis method, the equation of motion in the generalized coordinates is built upon the undamped eigenvalue data of the component structures. Error is inevitable when truncated modes are used. In this paper, two model truncation schemes were evaluated with regard to the critical speed, stability, and unbalance response of a two-spool gas turbine engine. The numbers of modes required to yield acceptable accuracy in these cases were determined. Guidelines for modal truncation were derived from these results.

Copyright © 1982 by ASME
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