ML18270A092: Difference between revisions
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{{#Wiki_filter:EXPLORING CAPABILITIES OF | {{#Wiki_filter:EXPLORING CAPABILITIES OF XFEM FOR USE IN FLAW EVALUATIONS Public Meeting 9/24/2018 Giovanni Facco RES/DE/CIB 1 | ||
-Motivation, Plan, Preliminary Results | |||
- | Objectives Introduce Plan to Investigate Use of xFEM Methods to Investigate PWSCC Growth | ||
- Motivation, Plan, Preliminary Results | |||
- Feedback Discuss International Efforts/Collaboration 2 | |||
Motivation | Motivation | ||
*RES has identified that future PWSCC flaw evaluations may involve 3D Finite Element Models of crack growth with complex stresses in asymmetrical components. | * RES has identified that future PWSCC flaw evaluations may involve 3D Finite Element Models of crack growth with complex stresses in asymmetrical components. | ||
*In order to be able to properly evaluate this kind of model RES plans to continue building upon its computational expertise in this potentially regulatory significant area. | * In order to be able to properly evaluate this kind of model RES plans to continue building upon its computational expertise in this potentially regulatory significant area. | ||
*Developing these capabilities and sharing what we learn we hope to improve and modernize how these issues are evaluated in the future 3 | * Developing these capabilities and sharing what we learn we hope to improve and modernize how these issues are evaluated in the future 3 | ||
Current FEA Application | Current FEA Application | ||
-Model WRS in complex geometries by simulating weld parameters 1.Perform thermal analysis 2.Impose thermal history in mechanical analysis to generate WRS profile | - Model WRS in complex geometries by simulating weld parameters | ||
-Multiple weld histories can be explored without the need for new model or re | : 1. Perform thermal analysis | ||
-meshing-These Results can then be used to calculate crack growth | : 2. Impose thermal history in mechanical analysis to generate WRS profile | ||
Traditional FEA vs | - Multiple weld histories can be explored without the need for new model or re-meshing | ||
*Results in very accurate SIF and stress states | - These Results can then be used to calculate crack growth rates No Repair OD Repair No Repair OD Repair Root Repair Large ID Repair Root Repair Large ID Repair 4 Thermal Model Mechanical Model | ||
*Requires re | |||
-meshing for any | Traditional FEA vs xFEM Traditional FEA xFEM | ||
* Results in very accurate SIF and | |||
*Can quickly calculate SIF of multiple cracks and crack lengths without major modifications to model | * Mesh-independent analysis of stress states discontinuities and singularities | ||
*Can model realistic 3D crack growth without re | * Requires re-meshing for any | ||
- | * Can quickly calculate SIF of multiple change crack size or geometry cracks and crack lengths without major | ||
* Analysis usually limited to modifications to model idealized crack shapes and planar | |||
* Can model realistic 3D crack growth crack growth due to complexity of without re-meshing models Traditional FEA Crack Growth 5 | |||
Current Crack Growth Rate Methods | Current Crack Growth Rate Methods | ||
*Crack growth calculations based on ASME Methodology | * Crack growth calculations based on ASME Methodology | ||
-2D approximations | - 2D approximations | ||
-Uses idealized crack shape and growth model (semi | - Uses idealized crack shape and growth model (semi-elliptical) | ||
-elliptical | - Assumes planar crack growth, perpendicular to pipe wall | ||
- WRS profile for crack growth is path dependent and user defined 6 | |||
-WRS profile for crack growth is path dependent and user defined 6 Research Project | |||
-Reproduce PWSCC Growth Behaviors-Investigate Cracking Property Response | Research Project Plan PWSCC Crack Growth Development | ||
-Investigate Simulation Parameter | - Reproduce PWSCC Growth Behaviors | ||
-Develop material property relationships using experimental component geometry (e.g. C(T) Specimen) to benchmark model response. | - Investigate Cracking Property Response | ||
Industry Relevant Models-Compared | - Investigate Simulation Parameter Response Model Material Behavior | ||
7 Methodology | - Develop material property relationships using experimental component geometry (e.g. C(T) | ||
*ABAQUS can simulate fatigue crack growth using a Paris Law type relationship=*ASME Code analysis determines PWSCC crack growth behavior using a similar power law relationship=*G and K are interrelated by a linear relationship in LEFM=where E'=E for plane stress and = | Specimen) to benchmark model response. | ||
*In cooperation with Committee on the Safety of Nuclear Installations (CSNI) the NRC is taking part in a technical round robin project exploring X | Industry Relevant Models | ||
-FEM Capabilities. | - Compared xFEM results to similar industry relevant models evaluated using traditional methods. | ||
-Multinational group (Public and Private, 12 Countries) | 7 | ||
-Focus is on an preliminary comparison of the X-FEM capabilities of the different codes used in the nuclear industry-Goal is to share Methodology and Results in order to evaluate capabilities and develop best practices. | |||
11 International Benchmarking Efforts | Methodology | ||
*Three benchmark problems | * ABAQUS can simulate fatigue crack growth using a Paris Law type relationship | ||
-Surface Crack in Plate | |||
-Embedded Crack in Plate Subjected to Shear Load | = | ||
-Underclad Crack in Core Shell of an RPV*Evaluate stationary cracks | * ASME Code analysis determines PWSCC crack growth behavior using a similar power law relationship | ||
*Thermal and mechanical loading*Static and transient conditions 12 Summary*Developing | |||
-Investigate Use of | = | ||
* G and K are interrelated by a linear relationship in LEFM 2 | |||
= | |||
where E'=E for plane stress and = for plane strain (12 ) | |||
8 | |||
Initial Results Stress Intensity Factor Calculations Fatigue Crack Growth 2D Single Edge Notch (Video) | |||
= | |||
Comparison of Nondimensional Stress Intensity Factors Contour ABAQUS RES % % Error (Handbook Benchmark Model Difference Value of 2.826) 2 2.8537 2.8712 0.61098 1.599 3 2.9643 2.9815 0.57967 5.504 4 3.0027 2.9956 0.23679 6.001 5 2.9696 2.9726 0.10218 5.189 9 | |||
Status | |||
* Successfully used ABAQUS simplified fatigue crack growth method, to grow a crack in a static stress field (externally applied or internal) in a 2D model | |||
* Developed preliminary parameter relationships between ABAQUS fatigue model and PWSCC model | |||
* Cracking parameter response (G & K) for 2D models shows good agreement with handbook values 10 | |||
International Benchmarking Efforts | |||
* In cooperation with Committee on the Safety of Nuclear Installations (CSNI) the NRC is taking part in a technical round robin project exploring X-FEM Capabilities. | |||
- Multinational group (Public and Private, 12 Countries) | |||
- Focus is on an preliminary comparison of the X-FEM capabilities of the different codes used in the nuclear industry | |||
- Goal is to share Methodology and Results in order to evaluate capabilities and develop best practices. | |||
11 | |||
International Benchmarking Efforts | |||
* Three benchmark problems | |||
- Surface Crack in Plate | |||
- Embedded Crack in Plate Subjected to Shear Load | |||
- Underclad Crack in Core Shell of an RPV | |||
* Evaluate stationary cracks | |||
* Thermal and mechanical loading | |||
* Static and transient conditions 12 | |||
Summary | |||
* Developing xFEM Techniques | |||
- Investigate Use of xFEM for PWSCC Growth | |||
- International Collaboration Efforts | |||
* Feedback 13}} | |||
Revision as of 14:03, 20 October 2019
| ML18270A092 | |
| Person / Time | |
|---|---|
| Issue date: | 09/24/2018 |
| From: | Giovanni Facco NRC/RES/DE/CIB |
| To: | |
| Michael Benson | |
| Shared Package | |
| ML18270A088 | List: |
| References | |
| Download: ML18270A092 (13) | |
Text
EXPLORING CAPABILITIES OF XFEM FOR USE IN FLAW EVALUATIONS Public Meeting 9/24/2018 Giovanni Facco RES/DE/CIB 1
Objectives Introduce Plan to Investigate Use of xFEM Methods to Investigate PWSCC Growth
- Motivation, Plan, Preliminary Results
- Feedback Discuss International Efforts/Collaboration 2
Motivation
- RES has identified that future PWSCC flaw evaluations may involve 3D Finite Element Models of crack growth with complex stresses in asymmetrical components.
- In order to be able to properly evaluate this kind of model RES plans to continue building upon its computational expertise in this potentially regulatory significant area.
- Developing these capabilities and sharing what we learn we hope to improve and modernize how these issues are evaluated in the future 3
Current FEA Application
- Model WRS in complex geometries by simulating weld parameters
- 1. Perform thermal analysis
- 2. Impose thermal history in mechanical analysis to generate WRS profile
- Multiple weld histories can be explored without the need for new model or re-meshing
- These Results can then be used to calculate crack growth rates No Repair OD Repair No Repair OD Repair Root Repair Large ID Repair Root Repair Large ID Repair 4 Thermal Model Mechanical Model
Traditional FEA vs xFEM Traditional FEA xFEM
- Results in very accurate SIF and
- Mesh-independent analysis of stress states discontinuities and singularities
- Requires re-meshing for any
- Can quickly calculate SIF of multiple change crack size or geometry cracks and crack lengths without major
- Analysis usually limited to modifications to model idealized crack shapes and planar
- Can model realistic 3D crack growth crack growth due to complexity of without re-meshing models Traditional FEA Crack Growth 5
Current Crack Growth Rate Methods
- Crack growth calculations based on ASME Methodology
- 2D approximations
- Uses idealized crack shape and growth model (semi-elliptical)
- Assumes planar crack growth, perpendicular to pipe wall
- WRS profile for crack growth is path dependent and user defined 6
Research Project Plan PWSCC Crack Growth Development
- Reproduce PWSCC Growth Behaviors
- Investigate Cracking Property Response
- Investigate Simulation Parameter Response Model Material Behavior
- Develop material property relationships using experimental component geometry (e.g. C(T)
Specimen) to benchmark model response.
Industry Relevant Models
- Compared xFEM results to similar industry relevant models evaluated using traditional methods.
7
Methodology
- ABAQUS can simulate fatigue crack growth using a Paris Law type relationship
=
=
- G and K are interrelated by a linear relationship in LEFM 2
=
where E'=E for plane stress and = for plane strain (12 )
8
Initial Results Stress Intensity Factor Calculations Fatigue Crack Growth 2D Single Edge Notch (Video)
=
Comparison of Nondimensional Stress Intensity Factors Contour ABAQUS RES % % Error (Handbook Benchmark Model Difference Value of 2.826) 2 2.8537 2.8712 0.61098 1.599 3 2.9643 2.9815 0.57967 5.504 4 3.0027 2.9956 0.23679 6.001 5 2.9696 2.9726 0.10218 5.189 9
Status
- Successfully used ABAQUS simplified fatigue crack growth method, to grow a crack in a static stress field (externally applied or internal) in a 2D model
- Developed preliminary parameter relationships between ABAQUS fatigue model and PWSCC model
- Cracking parameter response (G & K) for 2D models shows good agreement with handbook values 10
International Benchmarking Efforts
- In cooperation with Committee on the Safety of Nuclear Installations (CSNI) the NRC is taking part in a technical round robin project exploring X-FEM Capabilities.
- Multinational group (Public and Private, 12 Countries)
- Focus is on an preliminary comparison of the X-FEM capabilities of the different codes used in the nuclear industry
- Goal is to share Methodology and Results in order to evaluate capabilities and develop best practices.
11
International Benchmarking Efforts
- Three benchmark problems
- Surface Crack in Plate
- Embedded Crack in Plate Subjected to Shear Load
- Underclad Crack in Core Shell of an RPV
- Evaluate stationary cracks
- Thermal and mechanical loading
- Static and transient conditions 12
Summary
- Developing xFEM Techniques
- Investigate Use of xFEM for PWSCC Growth
- International Collaboration Efforts
- Feedback 13