Funder
National Major Science and Technology Projects of China
Aeronautical Science Foundation of China
National Science and Technology Major Project
National Natural Science Foundation of China
Reference69 articles.
1. Review on dynamic modeling and vibration characteristics of rotating cracked blades;Ma;J. Dyn. Monit. Diagn.,2023
2. B. Tudes, Rub Induced Rotor/Stator Vibration Analysis on CF700 engine, National Research Council Canada, Institute for Mechanical Engineering, Technical Report 1991/01, TR-ENG-007, pages 1-71. https://aeroenginesafety.tugraz.at/doku.php?id=7:71:713:713.
3. A transfer matrix method capable of determining the exact solutions of a twisted Bernoulli–Euler beam with multiple edge cracks;Lee;Appl. Math. Model.,2017
4. Free vibration analysis of a rotating graphene nanoplatelet reinforced pre-twist blade-disk assembly with a setting angle;Zhao;Appl. Math. Model.,2021
5. Nonlinear dynamic analysis of parked large wind turbine blade considering harmonic inertial excitation using continuum mathematical model;Jiang;Thin-Walled Struct.,2022
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