AE610 : Aircraft Vibration and Structural Dynamics

Department

Department of Aeronautical Engineering

Academic Program

Master in Master of Aerospace Engineering

Type

Compulsory

Credits

03

Prerequisite

Overview

Review of Single and Multi-degree of freedom vibration systems using matrixformulation and force methods, Lagrange’s equation for multi-degree free and forcedsystems, Time and frequency domain solution techniques. Vibration isolation dampingtreatment and dynamic absorbers. Analysis of Continuous systems: longitudinalvibration of rods, torsional vibration of rods, Euler equation for the beam, vibration ofmembranes, approximate numerical methods: Rayleigh method, dunkerley’s equation,matrix iteration method, calculation of higher modes of vibration systems. Vibrationmeasurement and analysis techniques.