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Blade loss transient dynamics analysis, volume 1. Task 2: TETRA 2 theoretical developmentThe 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.
Document ID
19880001409
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gallardo, Vincente C.
(General Electric Co. Cincinnati, OH, United States)
Black, Gerald
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:179632
NASA-CR-179632
Accession Number
88N10791
Funding Number(s)
CONTRACT_GRANT: NAS3-24381
PROJECT: RTOP 505-33-7B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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