@inproceedings{30109dd8f5ba4e2792d981df04204e37,
title = "Vibration fatigue of turbine blade for liquid rocket engine",
abstract = "Turbine blades of rocket engines undergo severe vibration load during service, and fatigue could cause failure of the entire engine. Therefore it is important to predict vibration fatigue life of blades during design process. Theoretical model of multiaxial continuum damage mechanics is applied to calculate damage evolution. Modal analysis and harmonic response analysis are used to structural fatigue life under sinusoidal vibration load. The proposed method is effective and could be easily extended in other mechanical structures.",
author = "Yi Li and Bing Sun and Jie Fang and Tong Liang",
note = "Publisher Copyright: {\textcopyright} 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018 ; Conference date: 08-01-2018 Through 12-01-2018",
year = "2018",
doi = "10.2514/6.2018-1226",
language = "英语",
isbn = "9781624105326",
series = "AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials",
}