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On Force Control of an Engine Order–Type Excitation Applied to a Bladed Disk With Underplatform Dampers
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The paper presents an original multiple excitation system based on electromagnets with force control. The system is specifically designed in order to investigate the dynamics of bladed disks, since it mimics the excitation ...
Modeling the Microslip in the Flange Joint and Its Effect on the Dynamics of a Multistage Bladed Disk Assembly
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The complex architecture of aircraft engines requires demanding computational efforts when the dynamic coupling of their components has to be predicted. For this reason, numerically efficient reduced-order models (ROM) ...
Experimental Joint Identification Using System Equivalent Model Mixing in a Bladed Disk
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A joint between two components can be seen as a means to transmit dynamic information from one side to the other. To identify the joint, a reverse process called decoupling can be applied. This is not as straightforward ...
Reduced Order Modeling for Multistage Bladed Disks With Friction Contacts at the Flange Joint
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Most aircraft turbojet engines consist of multiple stages coupled by means of bolted flange joints which potentially represent source of nonlinearities due to friction phenomena. Methods aimed at predicting the forced ...