Accelerated Multifidelity Emulator Modeling for Probabilistic Rotor Response Study

Author:

Bae Harok1,Boyd Ian M.1,Carper Emily B.2,Brown Jeff2

Affiliation:

1. MME Department, Wright State University, 3640 Colonel Glenn Hwy, Dayton, OH 45435

2. Air Force Research Laboratory, Wright-Patterson, AFB 45433

Abstract

Abstract This paper presents an efficient methodology to build a modal solution emulator for the probabilistic study of geometrically mistuned bladed rotors by using the newly developed localized-Galerkin multifidelity (LGMF) modeling and eigensolution reanalysis (ER) with the symmetric successive matrix inversion (SSMI) methods. The key idea of the mistuned blade emulator is to establish a reduced functional relationship between the stochastic geometric variations and the disturbed modal responses. The prediction accuracy of an emulator generally depends on how many training samples of modal solutions are available and how well the potential modal switching due to stochastic mistuning is captured. To reduce the computational costs of generating training samples without sacrificing accuracy, this paper introduces the collaborative framework of the new approaches of multifidelity (MF) modeling and ER. The proposed framework is demonstrated for its computational benefits with several numerical examples including the point-cloud scanned mistuned blade problem.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference22 articles.

1. Assessment of Probabilistic Methods for Mistuned Bladed Disk Vibration,2005

2. Reduced-Order Model Development for Airfoil Forced Response;Int. J. Rotating Mach.,2008

3. A Fleet Risk Prediction Methodology for Mistuned IBRs Using Geometric Mistuning Models,2015

4. Mistuned Rotor Reduced Order Modeling With Surrogate-Modeled Airfoil Substructures,2017

5. Survey of Multifidelity Methods in Uncertainty Propagation, Inference, and Optimization,2016

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