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Some concept of Wind Engineering are Aeroelastic Effects, Along-Wind Dynamic Response, Antennas and Open-Frame Structures, Atmospheric Boundary Layers and Turbulence, Atmospheric Boundary, Basic Bluff-Body Aerodynamics. Main points of this lecture are: Basic Structural Dynamics, Sinusoidal Excitation, Random Excitation, Freedom Structures, Dynamics of Structures, Structural Dynamics, Structural Dynamics, Freedom System, Expressed As Percentage, Damping to Critical
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Basic structural dynamics I
For free vibration:
m 1 x 1 k 11 x 1 k 12 x 2 k 13 x 3 .......k1nxn 0
m 2 x 2 k 21 x 1 k 22 x 2 k 23 x 3 .......k2nxn 0
m (^) n xn kn1x 1 kn2x 2 kn3x 3 .......knnxn 0
mass m 1 :
mass m 2 :
mass mn:
Note coupling terms (e.g. terms in x 2 , x 3 etc. in first equation) stiffness terms k 12 , k 13 etc. are not necessarily equal to zero
Basic structural dynamics I
In matrix form : Assuming harmonic motion : {x }= {X}sin(t+)
This is an eigenvalue problem for the matrix [k]-1[m]
Basic structural dynamics I
Number of modes, frequencies = number of masses = degrees of freedom
Mode 2
m 1
m 2
m 3
mn
m 1
m 2
m 3
mn
Mode 1 Mode 3
m 1
m 3
mn
m 2
m 1
m 2
m 3
mn
x 1
xn
x 3 x 2
Pn
P 3 P 2 P 1
m 1 x 1 k 11 x 1 k 12 x 2 k 13 x 3 .......k1nxn p 1 (t)
m 2 x 2 k 21 x 1 k 22 x 2 k 23 x 3 .......k2nxn p 2 (t)
m (^) n xn kn1x 1 kn2x 2 kn3x 3 .......knnxn pn(t)
m 1 x 1 k 11 x 1 k 12 x 2 k 13 x 3 .......k1nxn p 1 (t)
m 2 x 2 k 21 x 1 k 22 x 2 k 23 x 3 .......k2nxn p 2 (t)
m (^) n xn kn1x 1 kn2x 2 kn3x 3 .......knnxn pn(t)
Each uncoupled equation is analogous to the equation of motion for a single d-o-f system, and can be solved in the same way
for i = 1, 2, 3…….n
mi
xi(t)
aj(t) is the generalized coordinate representing the variation of the response in mode j with time. It depends on time , not position
Assume that the response of each mass can be written as:
ij is the mode shape coordinate representing the position of the ith mass in the jth mode. It depends on position , not time
n
j 1
xi (t) ij.aj(t)
i = a 1 (t)
Mode 1
Mode 2
i
Mode 3
By substitution, the original equations of motion reduce to:
The matrix [G] is diagonal, with the jth term equal to :
The matrix [K] is also diagonal, with the jth term equal to :
Gj is the generalized mass in the jth mode
2 ij
n
i 1
j
2 j
2 ij
n
i 1
i
2
The right hand side is a single column, with the jth term equal to :
Pj(t) is the generalized force in the jth mode
n
i 1
ij
T
We now have a set of independent uncoupled equations. Each one has the form :
G a K a T p(t)
Gen. stiffness
This is the same in form as the equation of motion of a single d.o.f. system, and the same solutions for aj(t) can be used Docsity.com
We now have a set of independent uncoupled equations. Each one has the form :
This is the same in form as the equation of motion of a single d.o.f. system, and the same solutions for aj(t) can be used
G a K a T p(t)
Gen. force