Structural Dynamics-I Damping Viscous Damping, Coulomb Damping, and Hysteretic damping Reduces the response, Greater the damping, the greater the Reduction. Energy dissipated (into heat or radiated away) The loss of energy from the oscillatory system results in the decay of amplitude of free vibration. In steady-state forced vibration, the loss of energy is balanced by the energy which is supplied by the excitation.
Structural Dynamics-I Energy dissipated mechanism may emanate from Friction at supports and joints Hysteresis in material Elastic Wave Propagation Air resistance, fluid resistance Cracks in concrete Exact mathematical description is quite complicated MDOF-Damping Classical (Orthogonal, Proportional, or Modal) Damping Non-classical Damping
Structural Dynamics-I Damping in Structures
MDOF-Damping Structural Dynamics-I Sometime damping can be ignored, for example, if the force acts for relatively short time, a small amount of damping will not significantly affect the response Also, damping plays an insignificant role in steady state response of periodically forced system if the forcing frequency is not near one of the system responses.
MDOF-Damping Structural Dynamics-I For certain problems, it is better to solve directly the coupled differential equations instead of using the modal transformation. The damping matrix [c] is then needed.
MDOF-Damping Structural Dynamics-I
MDOF-Damping Structural Dynamics-I
MDOF-Damping Structural Dynamics-I
Structural Dynamics-I Mathematical model : Series of mass and stiffness proportional dampers. Since the mass matrix and the stiffness matrix are diagonalised by the mode shapes, so then would be any linear combination of the two. If the dampers (as shown) are given arbitrary (nonproportional) values, the damping matrix will not be uncoupled. A complex (imaginary number) eigenvalue problem would then be required. MDOF-Damping
Structural Dynamics-I Damping Models A dashpot is commonly used to represent the mechanism of structural damping. The dashpot has been tacitly combined with the spring in parallel. However, a number of combination dashpot and spring for dynamic systems have been proposed. The following s are the important
Structural Dynamics-I Damping Models The combination of dashpot and spring in parallel is called Voigt model, which is sometime is referred to as Kelvin model. Let the spring constant, damping coefficient . force applied to the system. and resulting deformation be denoted by respectively. S ince equal deformations arise in the Spring and the dashpot for a parallel model, the force are
Structural Dynamics-I Damping Models
Structural Dynamics-I Damping Models
Structural Dynamics-I Damping Models
Structural Dynamics-I Damping Models
Structural Dynamics-I Damping Models
Structural Dynamics-I Damping Models
Structural Dynamics-I Damping Models
Structural Dynamics-I Damping Models
Structural Dynamics-I Damping Models Although this model is apparently the same as Voigt model the damping coefficient c is assumed to be inversely proportional to the frequency w. Therefore, the expansion of equations follows Voigt model with the substitution of
Structural Dynamics-I Damping Models
Structural Dynamics-I Damping Models
Structural Dynamics-I Measurement of Damping
Structural Dynamics-I Measurement of Damping
Example MDoF -Rayleigh Damping CEng 6505
Example MDoF -Rayleigh Damping CEng 6505
Example MDoF -Rayleigh Damping CEng 6505
MDoF - Rayleigh Damping CEng 6505 DAMPING RATIO IN THE First AND Third MODES WILL BE 5 PERCENT OF CRITICAL.
Structural Dynamics-I Continuous, or distributed parameter systems are the systems in which inertia is continuously distributed throughout the system. A continuous system's dependent kinematic properties are functions of spatial variables, as well as time. Vibrations of continuous systems are governed by partial differential equations. Distributed Parameter (DP) Structures
Lumped Versus DP Structures Structural Dynamics-I p v CONTINUM MODEL
Structural Dynamics-I A Continuum Model Extends in all direction Has infinite particles, with continuous variation of material properties, deformation characteristics and stress state A Discrete Model is of finite size and is made up of an assemblage of substructures, components and members Distributed Parameter Systems Infinite Degree of Freedom Structure Lumped Versus DP Structures
Structural Dynamics-I Lumped Versus DP Structures
Equation of Motion Structural Dynamics-I EoM can be derived by Equilibrium of a differential element (convenient for most of the structures) Hamilton’s principle Lagrange's method Energy Methods For complex structures
Structural Dynamics-I Beams The beams have distributed mass and as such they have infinite degrees of freedom if their distributed mass is considered. Two Approaches: Exact Method -Analytical Method- Solving PDE Approximate Method - Emprical Method, Rayleigh’s Method, and Rayleigh Ritz Method
Structural Dynamics-I WAVE EQUATION : Free vibrations of certain one-dimensional systems are governed by the wave equation Beams
Structural Dynamics-I Beams
Structural Dynamics-I Exact Method
Structural Dynamics-I Exact Method
Structural Dynamics-I Free Vibration
Structural Dynamics-I Free Vibration
Structural Dynamics-I Example
Structural Dynamics-I Example
Structural Dynamics-I Example
Structural Dynamics-I Example
Structural Dynamics-I Plates Moment-Shear Force Resultants
Structural Dynamics-I Vibration of Plates Equation of Motion
Structural Dynamics-I Vibration of Plates BOUNDARY CONDITIONS
Structural Dynamics-I Vibration of Plates BOUNDARY CONDITIONS
Structural Dynamics-I Vibration of Plates BOUNDARY CONDITIONS-Free Edge There are three boundary conditions, whereas the equation of motion requires only two: Kirchhoff showed that the conditions on the shear force and the twisting moment are not independent and can be combined into only one boundary condition.
Structural Dynamics-I Vibration of Plates BOUNDARY CONDITIONS-Free Edge
Structural Dynamics-I Vibration of Plates BOUNDARY CONDITIONS-Free Edge
Structural Dynamics-I Vibration of Plates BOUNDARY CONDITIONS-Free Edge
Structural Dynamics-I Vibration of Plates FREE VIBRATION OF RECTANGULAR PLATES
Structural Dynamics-I Vibration of Plates FREE VIBRATION OF RECTANGULAR PLATES
Structural Dynamics-I Vibration of Plates FREE VIBRATION OF RECTANGULAR PLATES
Structural Dynamics-I Vibration of Plates Solution for a Simply Supported Plate
Structural Dynamics-I Vibration of Plates Solution for a Simply Supported Plate
Structural Dynamics-I Vibration of Plates Solution for a Simply Supported Plate
Structural Dynamics-I Vibration of Plates Solution for a Simply Supported Plate
Structural Dynamics-I Rayleigh’s Method
Structural Dynamics-I Rayleigh’s Method
Structural Dynamics-I Rayleigh-Ritz Method
Structural Dynamics-I Rayleigh-Ritz Method
Example- IDoF CEng 6505
CEng 6505 Example- IDoF
CEng 6505 Example- IDoF
CEng 6505 Example- IDoF
CEng 6505 Example-Rayleigh Method
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Structural Dynamics-I Summary
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Example-Rayleigh Method CEng 6505
Structural Dynamics-I Example
Structural Dynamics-I Summary
Structural Dynamics-I Example
Structural Dynamics-I Example
Structural Dynamics-I Example
Structural Dynamics-I Example
Structural Dynamics-I PDE for LONGITUDINAL FREE VIBRATION of BARS Example
Structural Dynamics-I Example
Structural Dynamics-I Example
Structural Dynamics-I Example
Structural Dynamics-I Example
Structural Dynamics-I Example
Structural Dynamics-I Example
Structural Dynamics-I Schedule S. No. Topic Date Day Timings Room 1 Last Lecture + Test 5 27 Jan Monday 9:00 PM ECR 2 Final Exam (CLOSE BOOK) Feb 10 Monday 9:00-12:00 AM ECR