Experimental investigation on dynamic response of flat blades with underplatform dampers-Reference-Cited by-同舟云学术

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Experimental investigation on dynamic response of flat blades with underplatform dampers

Published:2019-12 Issue:12 Volume:32 Page:2667-2678
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

ZHANG Dayi,GAO Bin,HONG Jie,FU Jianwei,GE Xiangyun

Funder

National Natural Science Foundation of China

Key Laboratory of Vibration and Control of Aero-Propulsion System

Ministry of Education

Northeastern University

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference36 articles.

1. A review of friction damping of turbine blade vibration;Griffin;Int J Turbo Jet Eng,1990

2. The forced response of shrouded fan stages;Menq;J Vib Acoust Stress Reliab Des,1986

3. Interfacial contact stiffness of fractal rough surfaces;Zhang;Sci Rep,2017

4. Panning L, Popp K, Sextro W. Asymmetrical underplatform dampers in gas turbine bladings: theory and application. ASME turbo expo 2004: Power for land, sea, and air; 2004 June 14-17; Vienna, Austria. New York: ASME; 2004. p. 269-80.

5. Vibration response analysis of blade-disk dovetail structure under blade tip rubbing condition;Ma;J Vib Control,2017

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical and Experimental Study on Dummy Blade with Underplatform Damper;Machines;2024-07-07

2. Numerical Simulation and Experimental Verification on the Effects of Vibration Suppression of HPT Blades;Lecture Notes in Electrical Engineering;2024

3. Experimental and Numerical Investigations on the Dynamic Response of Blades with Dual Friction Dampers;Aerospace;2023-11-22

4. Experimental Investigation of the Dynamic Response of a Flat Blade with Dual Dry Friction Dampers;Energies;2023-11-02

5. Nonlinear dynamics of turbine bladed disk with friction dampers: Experiment and simulation;International Journal of Mechanical Sciences;2023-11

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