Funder
National Major Science and Technology Projects of China
National Natural Science Foundation of China
Chinese Aeronautical Establishment Aeronautical Science Foundation
Reference72 articles.
1. A general geometrical theory of turbine blade underplatform asymmetric dampers;Gola;Mech. Syst. Signal Process,2023
2. Nonlinear dynamics of turbine bladed disk with friction dampers: experiment and simulation;Fantetti;Int. J. Mech. Sci.,2023
3. Vibration prediction of bladed disks coupled by friction joints;Malte;Arch. Comput. Method E.,2017
4. Validation of a turbine blade component test with frictional contacts by phase-locked loop and force-controlled measurements;Schwarz;J. Eng. Gas Turbines Power,2019
5. Influence of mesoscale friction interface geometry on the nonlinear dynamic response of large assembled structures;Yuan;Mech. Syst. Signal Process,2023
Cited by
2 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