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NASA NTRS · 19880001409

Blade loss transient dynamics analysis, volume 1. Task 2: TETRA 2 theoretical development

Abstract

The theoretical development of the forced steady state analysis of the structural dynamic response of a turbine engine having nonlinear connecting elements is discussed. Based on modal synthesis, and the principle of harmonic balance, the governing relations are the compatibility of displacements at the nonlinear connecting elements. There are four displacement compatibility equations at each nonlinear connection, which are solved by iteration for the principle harmonic of the excitation frequency. The resulting computer program, TETRA 2, combines the original TETRA transient analysis (with flexible bladed disk) with the steady state capability. A more versatile nonlinear rub or bearing element which contains a hardening (or softening) spring, with or without deadband, is also incorporated.

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BibTeXRIS

Gallardo, Vincente C., Black, Gerald. 1986-11-01. Blade loss transient dynamics analysis, volume 1. Task 2: TETRA 2 theoretical development. https://ntrs.nasa.gov/citations/19880001409

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