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STRUCTURAL
DYNAMICS
SEYE NIGUSSIE
Introduction
WHAT IS STRUCTURAL DYNAMICS ?
 Dynamics concerned with the study of force and motion which are
time dependent
 Methods for analyzing the stresses and deflection developed in any
given type of structure when it is subjected to an arbitrary dynamic
loading
 Dynamic load is any load of which its magnitude, direction , and/or
position varies with time.
 The structural response to a dynamic load , i.e., the resulting stresses
and deflection, is also time varying, or dynamic
 Two basically different approaches are available for evaluating
structural response to dynamic loads:(based on how loading is
defined )
1. Deterministic Analysis and
2. Nondeterministic Analysis
Dynamic Analysis Approaches
Deterministic Analysis
 The structural response i.e. displacement, acceleration ,velocity ,stress
etc., are completely known precisely as a function of time
 Requires prefect control over all the variables that influence the
properties and loadings
 Also known as prescribed dynamic loading
Nondeterministic Analysis
 The time variation of vibration is not completely known
 It provides only statistical information about the response statically
defined loading
 Also known as random dynamic loading
TYPES OF PRESCRIBED LOADINGS
 Classified in two categories , ‘ Periodic ‘ and ‘ Non-Periodic “
Periodic Loadings ;
 loads which exhibit the same time variation successively for the large number of cycles.
 The simplest form of periodic loading is a sinusoidal variation which termed as ‘simple
harmonic ‘
 e.g. hydrodynamic pressures generated by a propeller at the stern of a ship or by
inertial effects in reciprocating machinery
Cont..
Non-Periodic Loadings
 Loadings which doesn't exhibit the same time variation successively
 It may be short duration (blast or explosion ) or long duration
impulsive loadings (earthquake)
Comparison of static loading and dynamic
loading
i. In static problem load is constant while in dynamic problem the load and its
responses varies with respect to time
ii. Static problem has only one response ,i.e. displacement but dynamic problem
has three responses ,such as displacement, velocity and acceleration
iii. Static problem only one solution whereas a dynamic problem has infinite
umber of solutions which are time dependent in nature
iv. In static problem response can be calculated by the principle of force or
static equilibrium whereas in dynamic problem the response depend not only
upon the load but also upon the inertia force which oppose the acceleration
Causes of dynamic effects
 The most common types
a) Initial condition ; such as velocity and displacement produce dynamic effect in
the system e.g. the lift moving up and down suddenly stopped ,the cabin start to
vibrate
b) Applied force ; application of the external force e.g. bomb blast or wind force
on the building
c) Support motion ; the influence of support motion e.g. earthquake
Basic definitions
 Mass ; dynamically ,it is the property that describe how an unrestricted body
resist the application of an external force (W/g) kgs
 Stiffness ;force required to produce unite deformation or elastic property that
describe the level of resisting force that result when a body undergo a
change in length (N/m)
 Natural period ;time required to complete one cycle of free vibration
(second)
 Frequency ;number of cycles per unit time
 Natural frequency ; the number of frequency of free vibration
 Amplitude ; the maximum displacement or deformation of a vibrating system
from mean position
Basic definitions
 Free vibration ; vibration which persists in structure after the force causing
the motion has been removed
 Forced vibration ;the vibrating which maintained in a structure by steady
periodic force act on structure
 Fundamental mode of vibration ;the fundamental mode of vibration od a
structure is the mode having the lowest natural frequency
 Damping ;the resistance to the motion of vibrating body and the vibration
is called damped vibration(N/m/s)
 Resonance ;when the frequency of the external force ids equal or much
with one of the natural frequency of the vibrating system, the amplitude of
the vibrating system become excessively large
Type of vibration
1. Fee and Forced vibration
Free vibration ; vibration which persists in a structure after
the force causing the motion has been removed
Forced vibration ;vibration maintained in a structure by
steady periodic force acting on the structure
2. Damped and undamped vibration
damped vibration ;when there is no damping element
Undamped vibration ;when there is damping element
3. Linear and Non-Linear vibration ;
4. Deterministic and random vibration
5. Longitudinal, transversal and torsional vibration
DEGREE OF FREDOM
Degree of Freedom is the number of coordinates necessary to specify the
position or geometry of mass point at any instant during its vibration
 All real structures possess infinite number of dynamic degree of freedom.
 Depending on the independent coordinates required to describe the motion
,systems divided into three
a) single degree of freedom system(SDOF system)
b) Multiple degree of freedom system(MDOF system)
c) Continuous system
Single degree of freedom system(SDOF system)
If a single coordinate is sufficient to define the position or geometry of the
mass of the system at any instant of time
Multiple degree of freedom system(MDOF system)
If more than one independent coordinate is required to completely specify
the position or geometry of different masses of the system at any instant of time
Continuous system (distributed system)
If the mass of a system may be considered to be distributed over its entire
length, in which the mass is considered to have infinite degrees of freedom
METHODS OF DISCRETIZATION
 Lumped Mass Procedure
the distributed mass will be assumed as a
concentrated mass at discrete points
 Generalized Displacements
based on the assumption that the deflected
shape of the structure can be expressed as the sum
of a series of specified displacement patterns ; these
patterns then become the displacement
coordinates of the structure
 The Finite Element Concept
expressing the displacements of any given
structure in terms of a finite number of discrete
displacement coordinates, which combines certain
features of both the lumped mass and the
generalized coordinate procedures
FORMULATION OF THE EQUATIONS OF MOTION
The mathematical expressions defining the dynamic displacements are called the
equations of motion of the structure, and the solution of these equations of motion
provides the required displacement time histories
Direct Equilibration Using d'Alembert's Principle
 The equations of motion of any dynamic system represent expressions of Newton's
second law of motion, which states that the rate of change of momentum of any
mass particle m is equal to the force acting on it
 The concept that a mass develops an inertial force proportional to its acceleration
and opposing it is known as d'Alembert's principle.
Principle of Virtual Displacements
 If a system which is in equilibrium under the action of a set of externally
applied forces is subjected to a virtual displacement, i.e., a displacement
pattern compatible with the system's constraints, the total work done by the
set of forces will be zero
Variational Approach
 based on Hamilton's principle, makes no direct use of the inertial or
conservative forces acting in the system; the effects of these forces are
represented instead by variations of the kinetic and potential energies of the
system
CHAPTER ONE.pdf

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CHAPTER ONE.pdf

  • 2. Introduction WHAT IS STRUCTURAL DYNAMICS ?  Dynamics concerned with the study of force and motion which are time dependent  Methods for analyzing the stresses and deflection developed in any given type of structure when it is subjected to an arbitrary dynamic loading  Dynamic load is any load of which its magnitude, direction , and/or position varies with time.  The structural response to a dynamic load , i.e., the resulting stresses and deflection, is also time varying, or dynamic  Two basically different approaches are available for evaluating structural response to dynamic loads:(based on how loading is defined ) 1. Deterministic Analysis and 2. Nondeterministic Analysis
  • 3. Dynamic Analysis Approaches Deterministic Analysis  The structural response i.e. displacement, acceleration ,velocity ,stress etc., are completely known precisely as a function of time  Requires prefect control over all the variables that influence the properties and loadings  Also known as prescribed dynamic loading Nondeterministic Analysis  The time variation of vibration is not completely known  It provides only statistical information about the response statically defined loading  Also known as random dynamic loading
  • 4. TYPES OF PRESCRIBED LOADINGS  Classified in two categories , ‘ Periodic ‘ and ‘ Non-Periodic “ Periodic Loadings ;  loads which exhibit the same time variation successively for the large number of cycles.  The simplest form of periodic loading is a sinusoidal variation which termed as ‘simple harmonic ‘  e.g. hydrodynamic pressures generated by a propeller at the stern of a ship or by inertial effects in reciprocating machinery
  • 5. Cont.. Non-Periodic Loadings  Loadings which doesn't exhibit the same time variation successively  It may be short duration (blast or explosion ) or long duration impulsive loadings (earthquake)
  • 6. Comparison of static loading and dynamic loading i. In static problem load is constant while in dynamic problem the load and its responses varies with respect to time ii. Static problem has only one response ,i.e. displacement but dynamic problem has three responses ,such as displacement, velocity and acceleration iii. Static problem only one solution whereas a dynamic problem has infinite umber of solutions which are time dependent in nature iv. In static problem response can be calculated by the principle of force or static equilibrium whereas in dynamic problem the response depend not only upon the load but also upon the inertia force which oppose the acceleration
  • 7. Causes of dynamic effects  The most common types a) Initial condition ; such as velocity and displacement produce dynamic effect in the system e.g. the lift moving up and down suddenly stopped ,the cabin start to vibrate b) Applied force ; application of the external force e.g. bomb blast or wind force on the building c) Support motion ; the influence of support motion e.g. earthquake
  • 8. Basic definitions  Mass ; dynamically ,it is the property that describe how an unrestricted body resist the application of an external force (W/g) kgs  Stiffness ;force required to produce unite deformation or elastic property that describe the level of resisting force that result when a body undergo a change in length (N/m)  Natural period ;time required to complete one cycle of free vibration (second)  Frequency ;number of cycles per unit time  Natural frequency ; the number of frequency of free vibration  Amplitude ; the maximum displacement or deformation of a vibrating system from mean position
  • 9. Basic definitions  Free vibration ; vibration which persists in structure after the force causing the motion has been removed  Forced vibration ;the vibrating which maintained in a structure by steady periodic force act on structure  Fundamental mode of vibration ;the fundamental mode of vibration od a structure is the mode having the lowest natural frequency  Damping ;the resistance to the motion of vibrating body and the vibration is called damped vibration(N/m/s)  Resonance ;when the frequency of the external force ids equal or much with one of the natural frequency of the vibrating system, the amplitude of the vibrating system become excessively large
  • 10. Type of vibration 1. Fee and Forced vibration Free vibration ; vibration which persists in a structure after the force causing the motion has been removed Forced vibration ;vibration maintained in a structure by steady periodic force acting on the structure 2. Damped and undamped vibration damped vibration ;when there is no damping element Undamped vibration ;when there is damping element 3. Linear and Non-Linear vibration ; 4. Deterministic and random vibration 5. Longitudinal, transversal and torsional vibration
  • 11. DEGREE OF FREDOM Degree of Freedom is the number of coordinates necessary to specify the position or geometry of mass point at any instant during its vibration  All real structures possess infinite number of dynamic degree of freedom.  Depending on the independent coordinates required to describe the motion ,systems divided into three a) single degree of freedom system(SDOF system) b) Multiple degree of freedom system(MDOF system) c) Continuous system
  • 12. Single degree of freedom system(SDOF system) If a single coordinate is sufficient to define the position or geometry of the mass of the system at any instant of time
  • 13. Multiple degree of freedom system(MDOF system) If more than one independent coordinate is required to completely specify the position or geometry of different masses of the system at any instant of time Continuous system (distributed system) If the mass of a system may be considered to be distributed over its entire length, in which the mass is considered to have infinite degrees of freedom
  • 14. METHODS OF DISCRETIZATION  Lumped Mass Procedure the distributed mass will be assumed as a concentrated mass at discrete points  Generalized Displacements based on the assumption that the deflected shape of the structure can be expressed as the sum of a series of specified displacement patterns ; these patterns then become the displacement coordinates of the structure  The Finite Element Concept expressing the displacements of any given structure in terms of a finite number of discrete displacement coordinates, which combines certain features of both the lumped mass and the generalized coordinate procedures
  • 15. FORMULATION OF THE EQUATIONS OF MOTION The mathematical expressions defining the dynamic displacements are called the equations of motion of the structure, and the solution of these equations of motion provides the required displacement time histories Direct Equilibration Using d'Alembert's Principle  The equations of motion of any dynamic system represent expressions of Newton's second law of motion, which states that the rate of change of momentum of any mass particle m is equal to the force acting on it  The concept that a mass develops an inertial force proportional to its acceleration and opposing it is known as d'Alembert's principle.
  • 16. Principle of Virtual Displacements  If a system which is in equilibrium under the action of a set of externally applied forces is subjected to a virtual displacement, i.e., a displacement pattern compatible with the system's constraints, the total work done by the set of forces will be zero Variational Approach  based on Hamilton's principle, makes no direct use of the inertial or conservative forces acting in the system; the effects of these forces are represented instead by variations of the kinetic and potential energies of the system