Gaussian Stochastic Process Modeling of Blend Repaired Airfoil Modal Response Using Reduced Basis Mode Shape Approach
Author:
Affiliation:
1. Engine Integrity Branch, Turbine Engine Division, Aerospace Systems Directorate, Air Force Research Lab , Wright-Patterson AFB, OH 45433
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
https://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/144/9/091010/6909969/gtp_144_09_091010.pdf
Reference25 articles.
1. A Reduced-Order Model of Mistuning Using a Subset of Nominal System Modes;ASME J. Eng. Gas Turbines Power,2001
2. A Fundamental Model of Mistuning for a Single Family of Modes;ASME J. Turbomach.,2002
3. Uncertainties of an Automated Optical 3D Geometry Measurement, Modeling, and Analysis Process for Mistuend Integrally Bladed Rotor Reverse Engineering;ASME J. Eng. Gas Turbines Power,2013
4. Vibratory Parameters of Blades From Coordinate Measurement Machine Data;ASME. J. Turbomach.,2008
5. Reduced Order Modeling of a Bladed Rotor With Geometric Mistuning Via Estimated Deviations in Mass and Stiffness Matrices;ASME. J. Eng. Gas Turbines Power,2013
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