Convergence predictions for aeroelastic calculations of tuned and mistuned bladed disks-Reference-Cited by-同舟云学术

Convergence predictions for aeroelastic calculations of tuned and mistuned bladed disks

Published:2008-07 Issue:5 Volume:24 Page:732-749
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

He Z.,Epureanu B.I.,Pierre C.

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference31 articles.

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3. Bladh, J.R., 2001. Efficient predictions of the vibratory response of mistuned bladed disks by reduced order modeling. Ph.D. Thesis, The University of Michigan, Ann Arbor, MI.

4. Component-mode-based reduced order modeling techniques for mistuned bladed disks, Part I: theoretical models;Bladh;ASME Journal of Engineering for Gas Turbines and Power,2001

5. Component-mode-based reduced order modeling techniques for mistuned bladed disks, Part II: application;Bladh;ASME Journal of Engineering for Gas Turbines and Power,2001

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1. Closure to “Discussion of ‘Dynamic Modeling and Projection-Based Reduction Methods for Bladed Disks With Nonlinear Frictional and Intermittent Contact Interfaces’” (Wallaschek, J., Willeke, S., and Panning-von Scheidt, L., ASME Appl. Mech. Rev., 2019, 71(5), p. 055502);Applied Mechanics Reviews;2019-09-01

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3. Nonlinear Reduced Order Models for the Structural Dynamics of Combustor Systems With Prestress and Friction;Journal of Computational and Nonlinear Dynamics;2014-09-12

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5. Analyzing mistuned multi-stage turbomachinery rotors with aerodynamic effects;Journal of Fluids and Structures;2013-10