Download webinar_17_SDOF_force_python

Unit 17
Vibrationdata
SDOF Response to Applied Force
Revision A
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Introduction

SDOF systems may be subjected to an applied force

Modal testing, impact or steady-state force

Wind, fluid, or gas pressure

Acoustic pressure field

Rotating or reciprocating parts
Vibrationdata
Rotating imbalance
Shaft misalignment
Bearings
Blade passing frequencies
Electromagnetic force, magnetostriction
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Vibrationdata
SDOF System, Applied Force
m
= mass
c
= viscous damping coefficient
k
= stiffness
x
= displacement of the mass
f(t) = applied force
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Vibrationdata
Free Body Diagram
Summation of forces
f(t)
x
m
kx
 Fm x
m x   cx  kx  f ( t )
cx
(c / m)  2n
(k / m)  n 2
m x  cx  kx  f ( t )
c
k
1
x   x    x    f ( t )
m
m
m
x  2n x  n2 x 
1
f (t)
m
Solve using Laplace transform.
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For an arbitrary applied force, the displacement x is
Smallwood-type, ramp invariant, digital recursive filtering relationship
xi 
Vibrationdata
 2 exp  n T cosd T  x i 1
 exp  2n T x i  2








2exp  n T  cosd T  1  exp  n T  n 2 2  1 sin d T    n T  f i

3



m n T 
 d




1



n


2

 2 n T exp  n T  cosd T   21  exp  2n T   2
2  1 exp  n T sin d T  f i 1

3

m n T 
d

1





 n

2


2  1 sin d T   2 cosd T  f i  2
 2   n T  exp  2n T   exp  n T 

3

 d

m n T 



1
d   n 1 -  2

T = time step
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Vibrationdata
SDOF Acceleration
For an arbitrary applied force, the displacement x is
x i   2 exp  n T cosd T x i 1  exp  2n T x i  2

exp   n T sin d T 
m d T
 f i  2 f i 1  f i  2 
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Time Domain Calculation for Applied Force
Vibrationdata
Let
fn = 10 Hz
Q=10
mass = 20 lbm
Calculate response to applied force:
F = 4 lbf, freq = 10 Hz, 4 sec duration, 400 samples/sec
First:
vibrationdata > Generate Signal > Sine
Export time history as: sine_force.txt
Next: vibrationdata > Select Input Data Type > Force
> Select Analysis > SDOF Response to Applied Force
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Applied Force Time History
Vibrationdata
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Displacement
Vibrationdata
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Transmitted Force
Vibrationdata
Special case:
SDOF driven at resonance
Transmitted force
= ( Q )( applied force )
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Synthesize Time History for Force PSD
Vibrationdata
Frequency
(Hz)
Force
(lbf^2/Hz)
10
0.1
1000
0.1
Duration = 60 sec
Similar process to synthesizing a time history for acceleration PSD.
But the integrated force time history does not need to have a mean value of zero.
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Synthesized Time History for Force PSD
Vibrationdata
Export as:
force_th.txt
vibrationdata > Power Spectral Density > Force > Time History Synthesis from White Noise
f = 4.26 Hz
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Histogram of Force Time History
Vibrationdata
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PSD Verification
Vibrationdata
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SDOF Response
Vibrationdata
Let
fn = 400 Hz
Q=10
mass = 20 lbm
Calculate response to the previous synthesized force time history.
vibrationdata > Select Input Data Type > Force
> Select Analysis > SDOF Response to Applied Force
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Displacement
Vibrationdata
Export:
disp_resp_th.txt
Overall Level =
7.4e-05 in RMS
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Velocity
Vibrationdata
Export array:
vel_resp_th.txt
Overall Level =
0.18 in/sec RMS
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Acceleration
Vibrationdata
Export array:
accel_resp_th.txt
Overall Level = 1.3 GRMS
Crest Factor = 5.0
Theoretical Rayleigh
Distribution
Crest Factor = 4.6
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Transmitted Force
Vibrationdata
Export array:
tf_resp_th.txt
Overall Level =
24.3 lbf RMS
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Vibrationdata
Frequency Response Function
Dimension
Displacement/Force
Name
Admittance,
Compliance,
Receptance
Dimension
Force/Displacement
Name
Dynamic Stiffness
Velocity/Force
Mobility
Force/Velocity
Acceleration/Force
Accelerance,
Inertance
Force/Acceleration
Mechanical Impedance Apparent Mass,
Dynamic Mass
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FRF Estimators
H1  
G FX ()
G FF ()
Vibrationdata
Cross spectrum between force and response divided by
autospectrum of force
Cross spectrum is complex conjugate of first variable
Fourier transform times the second variable Fourier transform.
G FX ()   F * X
* Denotes complex conjugate
The response can be acceleration, velocity or displacement.
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FRF Estimators (cont)
H 2  
G XX ()
G XF ()
Vibrationdata
Autospectrum of response divided by cross spectrum between
response and force
Coherence Function  is used to assess linearity, measurement, noise, leakage error,
etc. Coherence is ideally equal to one.
2 
G FX ()
2
G XX ()  G FF ()
0  2  1
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Frequency Response Function Exercise
Vibrationdata
Calculate mobility function (velocity/force) using:
vibrationdata > miscellaneous > modal frf
- Two separate Arrays – Ensemble Averaging
Arrays: force_th.txt & vel_resp_th.txt
df = 3.91 Hz & use Hanning Window Important!
Plot H1 Freq & Mag & Phase
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Vibrationdata
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Mobility H1
SDOF fn=400 Hz, Q=10
Vibrationdata
Save Complex Array:
H1_mobility _complex.txt
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Mobility H2
SDOF fn=400 Hz, Q=10
Vibrationdata
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Coherence from Mobility
Vibrationdata
Coherence = 0.98
at 400 Hz
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Estimate Q from H1 Mobility, Curve-fit
Vibrationdata
fn=400 Hz
Q=10.1
H1_mobility _complex.txt
vibrationdata > Damping Functions > Half-power Bandwidth Curve-fit, Modal FRF
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Homework
Vibrationdata

Repeat the examples in the presentation using the Matlab scripts

Read:
•
T. Irvine, Machine Mounting for Vibration Attenuation, Rev B, Vibrationdata,
2000
•
Bruel & Kjaer Booklets:
Mobility Measurement
Modal Testing
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