A novel model reduction approach for blisks with blend repairs and small mistuning

Author:

Zhou Biao,Berruti Teresa Maria

Funder

National Natural Science Foundation of China

Horizon 2020 Framework Programme

Horizon 2020

H2020 Marie Skłodowska-Curie Actions

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,Aerospace Engineering,Civil and Structural Engineering,Signal Processing,Control and Systems Engineering

Reference29 articles.

1. Recent progress in turbine blade and compressor blisk regeneration;Aschenbruck;Proc. CIRP,2014

2. Consequences of borescope blending repairs on modern high pressure compressor blisk aeroelasticity;Hanschke;J. Turbomach.,2019

3. J.A. Beck, J.M. Brown, B. Runyon, O.E. Scott-Emuakpor, Probabilistic Study of Integrally Bladed Rotor Blends using Geometric Mistuning Models, in: 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Grapevine, Texas, US, 2017.

4. Optimization of airfoil blend limits with as-manufactured geometry finite element models;Brown,2020

5. Blisk with small geometry mistuning and blend repair: as-measured fe model and experimental verification;Zhou,2022

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