Post on 23-Jul-2022
AeroHydroPLUS1
End-to-end statistical modelfor maximum expected vibration response
under aero-acoustic loading
Paul Bremner
AeroHydroPLUS
Outline
• Motivation• Variation in flight test data• Ensemble Mean vibration response • Ensemble Variance in modal response• Total Variance of vibration response• Contributions to Total variance
2
AeroHydroPLUS
MotivationMaximum expected vibration under aero-acoustic loading
I. Vibration test specification for space flight vehicle equipment
II. Sonic fatigue of aircraft empennage
3
AeroHydroPLUS
Outline
• Motivation• Variation in flight test data• Ensemble Mean vibration response • Ensemble variance in vibration modes• Total variance of vibration response• Contributions to Total variance
4
AeroHydroPLUS
Variation in launch vehicle skin vibration levelsPredict maximum expected from Mean, Variance and PDF
5
NASA HDBK-7005 (A. Piersol Ch.6)• Different points on skin panel• Data from multiple flights
1.E-03
1.E-02
1.E-01
1.E+00
1.E+01
10 100 1000
Rel
ativ
e Va
rianc
e
Frequency (Hz)
RELATIVE VARIANCE
2
22 2 2Rev
lVar v v
0.2
52 297.5 1.96Log v Var Log vP Log v
97.5%
MEAN 2 2
, SpatialFlt fltMean v v
AeroHydroPLUS
Outline
• Variance [uncertainty] in flight test data• Ensemble Mean vibration response • Ensemble variance in vibration modes• Total variance of vibration response• Contributions to Total variance
6
AeroHydroPLUS
Vibration response to general random FSP load
7
– Temporal term: Modal receptance
– Modal joint acceptance
– Homog. cross spectrum of aeroacoustic loading
2 22 2
22, r o pp r
vv or r r
G jG A
m Y
xx
22
1( ) ( )G ( , ; ) ( )G ( )r r pp r
pp A
j d dA
x x x x x x
( , '; )pG x x
,vv oG x
22 rrrr iY
G ( , ; ) G ( ) cosy cx c c k yc k xpp pp ce e k x x x
Gpp (x,ω)
Gvv (x,ω)
AeroHydroPLUS
Mean vibration Energy levelOver ensemble of similar structures & uncertainty in loading
8
1. Surface integral (≡ average) for total energy
2. 2nd average over uncertain input pressure distribution and spatial correlation
3. Integrate (3rd average) over frequency band Δω
2 2 2
22 2 2 4i
pp r
xr
r r r r
A G jE
m
2 2
, 2i
pp r
xr
G j A rEm
Total Energy E 2ˆ ,
A
E m v d x x x
2 2 * *
*2 2 2 2
, ,
1 1
r r s s
r s r r r s s s
A P j P j d dE m
m j m j
x x x x x x
AeroHydroPLUS
Mean Power InputOver ensemble of similar structures & uncertainty in loading
9
1. Power input from modal expansion
2. Average over uncertain input pressure distribution and spatial correlation
3. Integrate (2nd average) over frequency band Δω
1. Surface integral (≡ average) for total energy
2. 2nd average over uncertain input pressure distribution and spatial correlation
3. Integrate (3rd average) over frequency band Δω
* *
2 2
, ,Re
1r r r rin
r r r r
j P j P j d d
m j
x x x x x x
2 2 * *
*2 2 2 2
, ,
1 1
r r s s
r s r r r s s s
A P j P j d dE m
m j m j
x x x x x x
2 2 2
22 2 2 4i
pp r
xr
r r r r
A G jE
m
2 2
, 2i
pp r
xr
G j A rEm
2 2
22 2 2 4
r pp rin
inr
r r r r
A G j
m
2 2
2 2,
Re2i
pp rpp r iix
G j A r A G j Mm
Power Input ΠinTotal Energy E 2ˆ ,
A
E m v d x x x *Re , ,ini i i
A
P j v j d x x x
AeroHydroPLUS
This is familiar SEA !
Power Input Πin
10
1. Power input from modal expansion
2. Average over uncertain input pressure distribution and spatial correlation
3. Integrate (2nd average) over frequency band Δω
* *
2 2
, ,Re
1r r r rin
r r r r
j P j P j d d
m j
x x x x x x
Total Energy E
1. Surface integral (≡ average) for total energy
2. 2nd average over uncertain input pressure distribution and spatial correlation
3. Integrate (3rd average) over frequency band Δω
2ˆ ,A
E m v d x x x
2 2 * *
*2 2 2 2
, ,
1 1
r r s s
r s r r r s s s
A P j P j d dE m
m j m j
x x x x x x
2 2 2
22 2 2 4i
pp r
xr
r r r r
A G jE
m
2 2
, 2ix
pp rG j A rm
E
rω η
*Re , ,ini i i
A
P j v j d x x x
2 2
22 2 2 4
r pp rin
inr
r r r r
A G j
m
2
,
2
2i
pp r
x
G j A rm
SEA mean response of ANY modal subsystem
2inΠ = ω η E = ω η m v
AeroHydroPLUS
Outline
• Variance [uncertainty] in flight test data• Ensemble Mean vibration response • Ensemble Variance in modal response• Total Variance of vibration energy• Contributions to Total variance
11
AeroHydroPLUS
2nd statistical moment - Variance
12
2
22
2 Re2r
iipp r rj A
Var E Var QG
pV Mm
ar j
2 1 2 222 2
1 1 1 1 1, , 2 tan ln 1 ln 12
r B B B BB B
mm m B
modal densityQm
Lyon 1969, Weaver 1989 and Langley 2004
• Modal overlap
• Relative bandwidth
• Loading spatial correlation variance
2
22 2, 0
2 22 2 2
Re
Re , ,
iiVar p Var Q
ii
Var E p Q Var j M
p Q j M r m B
/B Q
24 2r rE j E j
AeroHydroPLUS
Relative Variance of ensemble modal dynamicsr2 [E] = Var[E] / <E>2
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MEANVibration energy
REL. VARIANCEVibration energyMonte Carlo SIMULATION
with random masses
Laboratory TESTINGwith random masses
AeroHydroPLUS
Variance of distributed random loading
14
21 22
1 1, ,mm
r B F B F Bm
Monte Carlo SIMULATIONdistrib. load & random masses
Dirac Delta spatial correlation
Diffuse acoustics, TBL spatial correlation
4
22
11E j K
NE j
AeroHydroPLUS
Outline
• Variance [uncertainty] in flight test data• Ensemble Mean vibration response • Ensemble variance in vibration modes• Total variance of vibration response• Contributions to Total variance
15
AeroHydroPLUS
TOTAL Variance of vibration Energy
16
2 2
2 2 2 22 22 2 2 2 2 2
2 222 2 2 2 2 2
Re
Re Re Re
Re Re Re
s ii
s ii s ii ii s
s ii s ii ii s
Var E Var p Var Q Var j M
p Q Var j M p j M Var Q Q j M Var p
p Var Q Var j M Q Var p Var j M j M Var p Var Q
2 2 2 2 2 2
2 2 2 2 2 2 2 2 2 2 2 2 2 2 2
Re
Re Re Re
s ii
s ii s ii s ii
r E r p r Q r j M
r p r Q r Q r j M r p r j M r p r Q r j M
2 2 2 2 2 2j Res iir E r p r Q r M
2 1ir X 2 1ir X
2 2 Re iiE p j M Q Product of 3 statistically uncorrelated variables
AeroHydroPLUS
Spatial varianceDiscrete point response versus Energy level
• Energy
• Vibration at discrete point [Langley 2005]
17
2
2
ˆA
sp
E m v d
m v
x x x
x
2
2 2
2 2 2 2 2
2
2 Re
sp
s ii
v E m
Var v F B r E
F B r p r j M r Q
x
x 22r v
x
2r E
AeroHydroPLUS
Outline
• Variance [uncertainty] in flight test data• Ensemble Mean vibration response • Ensemble variance in vibration modes• Total variance of vibration response• Contributions to Total variance
18
AeroHydroPLUS
Measured Variance – FLUCT SURFACE PRESSUREAt different AoA and Azimuthal station
Transonic FSP
19 AeroHydroPLUS166th Meeting: Acoustical Society of America
1.E‐03
1.E‐02
1.E‐01
1.E+00
1.E+01
1 10 100 1000 10000
Relative
Variance
Frequency (Hz)
1.E+02
1.E+03
1.E+04
1.E+05
1.E+06
1.E+07
1 10 100 1000 10000
Mea
n Sq
. Pressure [Pa^
2]
Frequency (Hz)
Sta 14 M=0.9 Run 70 0°Sta 14 M=0.9 Run 70 45°Sta 14 M=0.9 Run 70 90°Sta 14 M=0.9 Run 70 135°Sta 14 M=0.9 Run 70 180°Sta 14 M=0.9 Run 70 225°Sta 14 M=0.9 Run 70 270°Sta 14 M=0.9 Run 70 315°Sta 14 M=0.9 Run 72 0°Sta 14 M=0.9 Run 72 45°Sta 14 M=0.9 Run 72 90°Sta 14 M=0.9 Run 72 135°Sta 14 M=0.9 Run 72 180°Sta 14 M=0.9 Run 72 225°Sta 14 M=0.9 Run 72 270°Sta 14 M=0.9 Run 72 315°Sta 14 M=0.9 Run 67 0°Sta 14 M=0.9 Run 67 45°Sta 14 M=0.9 Run 67 90°Sta 14 M=0.9 Run 67 135°Sta 14 M=0.9 Run 67 180°
AeroHydroPLUS
Measured Variance – DAMPING LOSS FACTORDLF = 1/Q
20 AeroHydroPLUS166th Meeting: Acoustical Society of America
e
PIAAV Test Panele
0.001
0.01
0.1
10 100 1000 10000
Damping
Loss Fa
ctor
Frequency (Hz)
Oper TFn FitModal TestMESAM 22‐25 secMESAM 37‐40 secT60 High DLFT60 Low DLFMEAN
0.001
0.01
0.1
1
10
10 100 1000 10000
Relative Va
rian
ce
Frequency (Hz)
AeroHydroPLUS
Predicted versus Measured Total VarianceModel also ranks the multiple sources of uncertainty
21
A. Piersol NASA HDBK-7005
Vibr
atio
nPS
D
(g^2
/Hz)
2 2 22 22Re2 iisV r p rar v j QB r MF
x
0.001
0.010
0.100
1.000
10.000
10 100 1000
Relative
Varianc
e
Frequency, Hz
RelVar_MEASRelVar_MODEL2r^2[p^2]2r^2[Q]2r^2[j^2 ReM]F(B)
AeroHydroPLUS
Prediction of P95 maximum expected PSDUsing Total Relative Variance model + LogNormal PDF
22
A. Piersol NASA HDBK-7005
Vibr
atio
nPS
D
(g^2
/Hz)
1.E‐05
1.E‐04
1.E‐03
1.E‐02
1.E‐01
1.E+00
10 100 1000
Autospectral Den
sity, g^
2/Hz
Frequency Hz
Mean_MEAS
P95_MEAS
P95_MODEL
2
10 102 2
22
10 2
10 5 1
43 1
vv
vv
v
Gvvv
ref vv
GL
vv
GL Log Logv G
LogG
AeroHydroPLUS
Summary
• End-to-end statistical model– Predicts Total variance of vibration response
• Relative contributions to Total varianceI. Variance in fluct. surface pressure (FSP) levelII. Uncertainty in FSP spatial correlation & modal parameters (BCs, etc.)III. Variance in dampingIV. Bandwidth of random RMS response
• LogNormal PDF assumption– Predicts P95 max. expected vibration response– P99.5 ? … [tbc]
23
AeroHydroPLUS
BACK-UP MATERIAL
pbremner@aerohydroplus.comPh: 619 977 4048
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AeroHydroPLUS
MotivationCorrect uncertainty margins for model-based design ?
Because:i. All three uncertainties are statistically independent ; RSS (3 variances) < SUM ( 3 variances)ii. Fatigue Life is a product of 3 uncertain (random) variables -> LOG Normal distribution
III. Uncertainty inFatigue failure models
I. Uncertainty in Aero & Acoustic loading
1 10 100 1000 10000Frequency (Hz)
Sta 14 M=0.9 Run 72 90°Sta 14 M=0.9 Run 72 135°Sta 14 M=0.9 Run 72 180°Sta 14 M=0.9 Run 72 225°Sta 14 M=0.9 Run 72 270°Sta 14 M=0.9 Run 72 315°Sta 14 M=0.9 Run 67 0°Sta 14 M=0.9 Run 67 45°Sta 14 M=0.9 Run 67 90°Sta 14 M=0.9 Run 67 135°Sta 14 M=0.9 Run 67 180°
Sta 14 M=0.9 Run 70 0°Sta 14 M=0.9 Run 70 45°Sta 14 M=0.9 Run 70 90°Sta 14 M=0.9 Run 70 135°Sta 14 M=0.9 Run 70 180°Sta 14 M=0.9 Run 70 225°Sta 14 M=0.9 Run 70 270°Sta 14 M=0.9 Run 70 315°Sta 14 M=0.9 Run 72 0°Sta 14 M=0.9 Run 72 45°Fl
uct.
Sur
face
Pre
ssur
e P
SD
(P
a^2/
Hz)
RM
S S
tress
(M
N/m
^2)
N Cycles to failure
9 7 6. Loading VA model SN dataMIN EXPECTED Fatigue Life MEAN Fatigue L dB dB dBife
II. Uncertainty inVibro-acoustics model
AeroHydroPLUS26
Maximum expected levelPredictable from PDF, Mean and Variance
Energy Schroeder Pressure (Vibration) Field
2
2
2
v
2 299.5 10.6P v
P P
0.597.5 1.96P Log E Log E Var Log E
243 1Var Log E Log r E
97.5%
Exponential PDF Log Normal PDF
2 2 ReE p j M Q
AeroHydroPLUS
Measured Variance – FLUCT SURFACE PRESSUREAt different AoA and Azimuthal station
Supersonic FSP
27 AeroHydroPLUS166th Meeting: Acoustical Society of America
1.E‐03
1.E‐02
1.E‐01
1.E+00
1.E+01
1 10 100 1000 10000Re
lative
Variance
Frequency (Hz)
1.E+02
1.E+03
1.E+04
1.E+05
1.E+06
1.E+07
1 10 100 1000 10000
Mea
n Sq
. Pressure [Pa^
2]
Frequency (Hz)
Sta 14 M=0.95 Run 57 45°Sta 14 M=0.95 Run 57 90°Sta 14 M=0.95 Run 57 135°Sta 14 M=0.95 Run 57 180°Sta 14 M=0.95 Run 57 225°Sta 14 M=0.95 Run 57 270°Sta 14 M=0.95 Run 57 315°Sta 14 M=0.95 Run 57 0°Sta 14 M=0.95 Run 57 45°Sta 14 M=0.95 Run 57 90°Sta 14 M=0.95 Run 57 135°Sta 14 M=0.95 Run 57 180°Sta 14 M=0.95 Run 57 225°Sta 14 M=0.95 Run 57 270°Sta 14 M=0.95 Run 57 315°Sta 14 M=0.95 Run 57 0°Sta 14 M=0.95 Run 57 45°Sta 14 M=0.95 Run 57 90°Sta 14 M=0.95 Run 57 135°Sta 14 M=0.95 Run 57 180°Sta 14 M=0.95 Run 57 225°
AeroHydroPLUS28
AeroHydroPLUS
Nasa NESC Mach 8 plume impingement aero-acousic & vibration test (PIAAV)
Tap Test - Linear
PIAAV Test – Non-Linear
AeroHydroPLUS
FE (Abaqus) evaluation – with & without non-linear elasticity at 171dB FPL loading
0 1.0 2.0 3.0 4.0 5.0
PIAAV “equivalent beam” center ACCELERATION
LINEAR model NON-LINEAR model
10E10
10E9
10E6
10E5
PSD (G2/Hz)
0 500 1000 1500 2000 2500 Frequency (Hz)
10E10
10E9
10E6
10E5
PSD (G2/Hz)
0 500 1000 1500 2000 2500 Frequency (Hz)
1.5E6
1.0E6
0 1.0 2.0 3.0 4.0 5.0 Time (s)
G-0.5E6
0.5E6
-1.0E6
-1.5E6
1.0E6
Time (s)
G
-0.5E6
0.5E6
-1.0E6