Reduced Order Geometric Mistuning Models using Principal Component Analysis Approximations-Reference-Cited by-同舟云学术

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Reduced Order Geometric Mistuning Models using Principal Component Analysis Approximations

Published:2016-01-01 Issue: Volume: Page:
ISSN:
Container-title:57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Henry Emily B.¹,Brown Jeffrey M.¹,Beck Joseph A.²

Affiliation:

1. Air Force Research Laboratory

2. Perceptive Engineering Analytics

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0706

Reference30 articles.

1. Uncertainty treatment in forced response calculation of mistuned bladed disk

2. Vibratory Parameters of Blades From Coordinate Measurement Machine Data

3. Forced Response of Bladed Disk Assemblies--A Survey

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1. Optimization of Airfoil Blend Limits With As-Manufactured Geometry Finite Element Models;Journal of Engineering for Gas Turbines and Power;2022-01-03

2. Related Disciplines and Advanced Topics;Synthesis Lectures on Mechanical Engineering;2022

3. Mistuned Rotor Reduced Order Modeling with Surrogate-Modeled Airfoil Substructures;58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2017-01-05

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