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NASA NTRS ยท 19780067374

Modal confidence factor in vibration testing

Abstract

The modal confidence factor (MCF) is a number calculated for every identified mode for a structure under test. The MCF varies from 0.00 for a distorted nonlinear, or noise mode to 100.0 for a pure structural mode. The theory of the MCF is based on the correlation that exists between the modal deflection at a certain station and the modal deflection at the same station delayed in time. The theory and application of the MCF are illustrated by two experiments. The first experiment deals with simulated responses from a two-degree-of-freedom system with 20%, 40%, and 100% noise added. The second experiment was run on a generalized payload model. The free decay response from the payload model contained 22% noise.

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BibTeXRIS

Ibrahim, S. R.. 1978-10-01. Modal confidence factor in vibration testing. https://ntrs.nasa.gov/citations/19780067374

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