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Detuning and Decoupling in Vibration Control by Ashish Singh is a document available to read on EtoBox.

This document discusses detuning and decoupling techniques to reduce vibration. Detuning involves changing system parameters like mass and stiffness to avoid resonance with excitation frequencies. Decoupling decreases the number of coupled resonators in a system. These techniques are applied in aircraft structure design by stiffening fuselage panels with stringers to create a periodically supported beam structure. This spreads out the natural frequencies of the structure into propagation and attenuation ban

Author
Ashish Singh
Language
EN