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Digital Twin Workshop

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Title: Impact of Parameter Variation on Damage Tolerance Analysis Estimates Author: Southwest Research Institute Last modified by: Harry Millwater – PowerPoint PPT presentation

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Title: Digital Twin Workshop


1
Digital Twin Workshop
  • Harry Millwater
  • University of Texas at San Antonio
  • Sept. 10-11, 2012

2
Topics
  • FAA Probabilistic Damage Tolerance Analysis
  • System Reliability Analysis
  • Sensitivity Methods

3
Damage Tolerance Methodology
Loading
EVD
RS
Insp 2
Insp 1
Time
Material Prop.
4
POF Calculations
Survival t-1
POF Flight t
5
EVD Results
Frechet Gumbel Weibull
6
EVD Results
Usage Location Scale Shape Distribution
Single Engine Unpress. Basic Inst. 14.49 1.75 0.01 Frechet
Single Engine Unpress. Personal 12.03 1.15 0.00 Gumbel
Single Engine Unpress. Executive 11.68 0.90 -0.04 Weibull
Twin Engine Unpress. Basic Inst. 13.93 1.42 0.00 Gumbel
Twin Engine Unpress. General 12.05 1.16 0.02 Frechet
Pressurized 13.41 1.26 0.02 Frechet
Agric/Special 12.07 0.94 -0.12 Weibull
Special Usage Survey 14.56 1.32 -0.05 Weibull
7
Probabilistic Modeling of Systems
POF contours
L. Domyancic, D. Sparkman, and H.R. Millwater, L.
Smith and D. Wieland, A Fast First-Order Method
for Filtering Limit States, 50th AIAA AIAA
Nondeterministic Approaches Conference, May 4-7,
2009, Palm Springs, CA, AIAA 2009-2260
8
Pair-wise Filtering Criteria
  • Pair-wise filtering neglect limit states that
    dont contribute significantly to the system POF
    relative to the dominant limit states

g1 dominant limit state, serves as a benchmark
9
Filtering Procedure
  • Pair-wise comparison of each limit state with
    dominant
  • Each limit state is assigned a filtering error,
    i.e. the relative error incurred if the limit
    state were filtered
  • is calculated using the bivariate normal
  • User decides how much error to allow and set
    tolerance
  • (typical values 1E-4 1E-6)

10
Second Order Bounds
  • Examine the cumulative effect of the filtered
    limit states using 2nd order bounds
  • Compare bounds from a) all limit states vs. b)
    only unfiltered limit states

11
Aircraft Model
  • Lower wing skin analyzed, 900 limit states

LS Beta Corr. Filt. Error
292 0.297 1 0
277 0.65 0.99 2.50E-04
256 0.949 0.98 2.20E-09
g1
  • Root radius Element 292 and 277 left unfiltered
    (?TOL 1E-6)
  • Bounds on entire system vs. only critical
    locations widen by 1E-5

12
Sensitivity Methods
  • Numerical Differentiation ()
  • Visual
  • Linear Regression
  • Score Function partial derivatives
  • Local probabilistic partial derivatives ()
  • Global Sensitivity Analysis

13
Local Prob. Sensitivity
14
ZFEM Complex Variable FE Method
15
Abaqus 2D Verification
Analytical
Abaqus
16
Strain Energy Release Rate
Double Cantilever Beam (DBC)
Exact 0.800
Exact 0.8
of Contours Perturbation Method Abaqus CTSE
20 Tip only 0.7914
8 Tip only 0.7918
4 Tip only 0.7914
17
Higher Order Sensitivities
Thick walled cylinder
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