Accession Number:
AD1078294
Title:
AS-Manufactured Modeling of a Mistuned Turbine Engine Compressor Evaluated Against Experimental Approaches
Descriptive Note:
Technical Report,22 Sep 2016,30 Jun 2019
Corporate Author:
Wright State University Dayton United States
Personal Author(s):
Report Date:
2019-06-01
Pagination or Media Count:
155.0
Abstract:
The resonant response of integrally bladed rotors at various modes and harmonic excitations is investigated in this work. Two AMM finite element models FEM were created of a 20-bladed IBR. Strain gages in as-manufactured models AMM using this method changes the IBRs predicted mistuning. AMMs generated via optical topography measurements and mesh morphing should be acquired using clean, non-strain gaged rotors or the material properties of strain gaged elements need to be altered to more accurately model the component.
Descriptors:
Subject Categories:
- Jet and Gas Turbine Engines