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Transcript of WS_2013_04_Advanced_Materials_Aerospace.pdf
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Aerospace Industry Multi-Scale Modeling of Composite Materials & Structures Dr. Jan Seyfarth Product Manager Digimat April 2013
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Copyright© e-Xstream engineering, 2013 2
Aerospace Industry A Very Short Introduction...
Digimat e-Xstream & Simulation Strategy Software
Materials Technology & Applications
From Materials to Structure Current Status and Ongoing Developments
Structures Technology & Applications
Summary
Aerospace Industry Multi-Scale Modeling of Composite Materials & Structures
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Digimat
e-Xstream engineering Simulation Strategy
Nonlinear Multi-Scale Simulation Platform
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Aerospace Industry Multi-Scale Modeling of Composite Materials & Structures
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Copyright© e-Xstream engineering, 2013 4
Who are we...? A MSC Software Company! Team of ~30 persons PhDs (~65%) MS & BS Engineering (~ 25%) Marketing, Finance & Admin (~10%)
+ TBH in 2013
Material experts Micromechanics about...
COMPOSITES
Amsterdam, October 2012
e-Xstream engineering Digimat
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Copyright© e-Xstream engineering, 2013 5
What are we concerned about? Inter-dependencies in the Design of a Composite Part
e-Xstream engineering Digimat
Structural design
influences processing
Manufacturing sets
local microstructure
Local microstructure
sets material
properties
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What do we do...? Multi-Scale! MICRO Material
MACRO Dumbbell Part
System Copyright© e-Xstream engineering, 2013 6
Micro- structure Material model
Part performance
Characterization
Process
System level
Simulation Strategy Digimat
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Material Related Design Challenges Manage Material Data Generate Data (Cost & Time of Test) Manage, Trace, Protect (IP) Comply (Regulation)
Model (composite) Materials, Part & Systems Nonlinearity: Progressive damage & failure Anisotropy Heterogeneity Process dependency
Use The optimal mix of material The Material(s) as a design parameter to innovate The optimal manufacturing process
Simulation Strategy Digimat
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Nonlinear Multiscale Modeling Platform
8 Copyright© e-Xstream engineering, 2013
Nonlinear Multi-Scale Simulation Platform Digimat
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Performance Stiffness Failure Fatigue
Technology
Linear/Nonlinear Mean Field/FEA Micro/Hybrid
Copyright© e-Xstream engineering, 2013 9
Nonlinear Multiscale Modeling Platform Holistic modeling Materials
Chopped Fibers: Short/Long Continuous Fibers Fillers
Physics
(Thermo-) Mechanical Thermal Conductivity Electric Conductivity
Manufacturing
Injection Compression Draping Fiber placement MuCell®
Nonlinear Multi-Scale Simulation Platform Digimat
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Nonlinear Multiscale Modeling Platform MICRO Virtual Material
MACRO Data management Reverse Engineering FEA Interfaces Mapping
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Material Engineering
Structural Engineering
Nonlinear Multi-Scale Simulation Platform Digimat
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Interfaces to MSC Nastran SOL 101 - linear Weak coupling [Nastran material card used] Including SOL 103 for vibration Including SOL 105 for buckling
SOL 400 - nonlinear Implicit Strong coupling [Digimat user subroutine]
SOL 700 - nonlinear Explicit Strong coupling [Digimat user subroutine]
11 Copyright© e-Xstream engineering, 2013
Available in 4.4.1
Specification phase
Under development
Nonlinear Multi-Scale Simulation Platform Digimat
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Materials
Composites
Materials Engineering Applications
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Aerospace Industry Multi-Scale Modeling of Composite Materials & Structures
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Copyright© e-Xstream engineering, 2013 13
A Vast Mix of Different Materials Metal (Alloys) Aluminium / Magnesium Molybdenum / Titanium / Tungsten
Reinforced Plastics Thermoplastics + Carbon fibers Epoxy + Glass / Carbon / Aramid fibers
Ceramics Titanium + SiC fibers
Composites Materials
Complex structures Pores
Stacking Weaving
Structure / Orientation
Random
Performance (Stiffness, failure, fatigue, ...) Anisotropy
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Digimat-FE Fast & Efficient Prediction of Composite Material Properties
14 Copyright© e-Xstream engineering, 2013
Materials Engineering Materials
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UD Composites Defects & influence of processing ISEMP Integrative Simulation and Engineering of Materials and Processes » Aims at the simulation of material details and not only the macroscopic overall properties
» Aims at considering manufacturing process by the simulation » Uses commercially available software tools
CHALLENGE
Processing of CFRP results in residual stresses in the material Residual stresses lead to micro-damage & failure of CFRP Goal is to simulate residual stresses of a carbon fiber composite material at the micro scale with realistic topology
Copyright© e-Xstream engineering, 2012 15
Applications Materials
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UD Composites Defects & influence of processing E.g. already generated in the material during processing
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Segmentation
Matrix enrichment
Pores
Delamination
Applications Materials
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UD Composites RVE Generation Periodic boundary conditions Enhanced flexibility 45° orientation » And other...
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Applications Materials
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UD Composites RVE Generation Fibers Stochastic Intersection with » Matrix » Voids
Voids Stochastic Complex shapes Clustering, control over » Position » Shape » Orientation
Copyright© e-Xstream engineering, 2012 18
[ 0° / 90° ]
fibers intersecting voids
complex shapes
Applications Materials
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UD Composites Curing effects Replacement experiment: Shrinkage due to temperature decrease
Copyright© e-Xstream engineering, 2012 19
Applications Materials
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UD Composites Curing effects Delamination due to change in orientation
Copyright© e-Xstream engineering, 2012 20
Applications Materials
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UD Composites Curing effects Crack propagation due to stochastic distribution of fibers
Copyright© e-Xstream engineering, 2012 21
Applications Materials
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Strategic Simulation Tool Digimat Recommended tool for investigations
Copyright© e-Xstream engineering, 2012 22
DIGIMAT enables us to perform in depth studies of complex and realistic
microstructures. As an invest into the future we base our simulation approach on the
DIGIMAT software, both for our research and the education of a new generation of
simulation engineers who will be experts in the modeling of materials.
Prof. Vasily Ploshikhin, Airbus endowed chair for Integrative Simulation and
Engineering of Materials and Processes (www.isemp.de)
Applications Materials
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Sandwich Panels
Micross - Stand-Alone Digimat Module Input Data @ micro and/or macro scale Fast Solution in less than 10 minutes Loading 3-Point & 4-Point Bending In-Plane Shear
Tuesday, 23 April 2013 23
Applications Materials
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Micross
Stand-alone module Definition of honeycomb core Definition of skin plies
Tuesday, 23 April 2013 24
Applications Materials
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Micross
Stand-alone module Visualization of results Failure indicators Skins: max. stress, Tsai-Wu, Tsai-Hill, Azzi-Tsai-Hill Core: shear, compression
Tuesday, 23 April 2013 25
Applications Materials
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From Materials to Structure
Critical Development Phase Materials Engineering
Current Status Ongoing Developments
Copyright© e-Xstream engineering, 2013 26
Aerospace Industry Multi-Scale Modeling of Composite Materials & Structures
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Digimat-MF Fast & Efficient Prediction of Composite Material Properties
27 Copyright© e-Xstream engineering, 2013
Output
Homogenization
DIGIMAT material model sensitive to composite microstructure
State-of-the-art homogenization methods
Per-phase material properties + microstructure information
Input
ar w [%]
matrix
filler
Materials Engineering From Materials to Structure
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Digimat-MX Material eXchange & Reverse Engineering
28 Copyright© e-Xstream engineering, 2013
Reverse Engineering
Input
Output
Calibrated DIGIMAT Material Model, stored in database and ready to be shared and used
Calibration of DIGIMAT models based on experimental data
Experimental data, DIGIMAT material models stored in database
Materials Engineering From Materials to Structure
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Multi-Scale Approach Top Down | Reverse Engineering
29
Critical Development Phase From Materials to Structure
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Multi-Scale Approach Bottom Up | Prediction of performance
30
Critical Development Phase From Materials to Structure
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Material Models - Standart (Thermo-) Elastic (Thermo-) Elastoplastic (Thermo-) Viscoelastic (Thermo-) Elasto-Viscoplastic
31
f(T)
TEMPERATURE
f( )
STRAIN RATES
High strain rates Creep
f(OT) ANISOTROPY
Current Status From Materials to Structure
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Material Models Advanced (Thermal) Creep Viscoelasticity Elasto-Viscoplasticity
32
time
aligned
VE Matrix Composite
TVE Matrix Composite G0, K0 and CTE Constant
TVE Matrix Composite G0 =G0 0 = K0
Current Status From Materials to Structure
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Stiffness Eshelby approach for UD & woven composites Mean field homogenization Glass fibers isotropic Carbon fibers transversely isotropic
33
Current Status From Materials to Structure
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Stiffness UD Composites RVE definition Layered microstructure
34
Current Status From Materials to Structure
Stiffness Failure
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Stiffness Woven Composites - Basic model Superposition of fibers
35
Current Status From Materials to Structure
Copyright© e-Xstream engineering, 2013
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Stiffness Woven Composites - Advanced model Realistic woven structure
36
yarn definition
woven modeler
Current Status From Materials to Structure
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Stiffness Woven Composites - Advanced model
Realistic woven structure
37
visualization & property computation
Current Status From Materials to Structure
Copyright© e-Xstream engineering, 2013
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Stiffness Virtual testing Stress & strain Tension & compression Creep & relaxation
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uniaxial
shear
biaxial
Current Status From Materials to Structure
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Stiffness Input / Definition Epoxy matrix Density Isotropic elastic » modulus » Poisson ratio
Carbon fibers Density Transversely isotropic elastic » In-plane modulus » Axial modulus » In-plane Poisson ratio » Transverse Poisson ratio » Transverse shear modulus
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Current Status From Materials to Structure
ksi
t/mm3
ksi
t/mm3
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Stiffness Input / Definition Ply Microstructure » Continuous fiber » Volume fraction of fibers: 61%
Laminate Stacking sequence » 3 different laminates Computation of » Laminate
» Stress response » Engineering properties
» Ply » Engineering properties
» Per-phase » Stress response
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Current Status From Materials to Structure
10/30/60 Laminate 1
60/30/10 Laminate 2
10/40/50 Laminate 3
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Stiffness Output Laminate Stress response
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Current Status From Materials to Structure
11
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Stiffness Output Laminate Stiffness matrix » In coordinate system of the RVE » Tensile direction: 11 » Orthotropic
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Current Status From Materials to Structure
Laminate 1 10/30/60
Laminate 2 60/30/10
Laminate 3 10/40/50
11
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Stiffness Output Ply level Engineering constants » In coordinate system of the ply » Tensile direction: x » Unique for all three laminates
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Current Status From Materials to Structure
Lamina Angle 0° 45° 90°
Young Modulus (ksi)
Axial (along x-‐axis) 23.044 2.139 1.318
Transverse (along y-‐axis) 1.318 2.139 23.044
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Stiffness Output Matrix level Microscopic properties » Stress 11 vs. Strain 11 [ksi] Per ply information » Different stresses ( ) & strains are reached » Dependent on the ply and sensitive to changes in the laminate design
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Current Status From Materials to Structure
imposed strain imposed strain imposed strain
0° 45° 90°
matrix strain matrix strain matrix strain
11
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Stiffness Output Fiber level Microscopic properties » Stress 11 vs. Strain 11 [ksi] Per ply information » Dependent on the ply and sensitive to changes in the laminate design
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Current Status From Materials to Structure
imposed strain imposed strain imposed strain fiber strain fiber strain fiber strain
11
0° 45° 90°
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Stiffness Coupled Analysis
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Current Status From Materials to Structure
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Stiffness Coupled Analysis Global Response Laminate level Force / displacement curve » Digimat-MF Fraction of a second to solve micromechanics » Nastran Minutes for FEA analysis
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Current Status From Materials to Structure
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Stiffness Coupled Analysis Local Response Ply level Macroscopic properties in each ply » Max. Princ. Stress [ksi] » Influence of the hole on local behavior
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Current Status From Materials to Structure
Laminate 1 10/30/60
Laminate 2 60/30/10
Laminate 3 10/40/50
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Failure Matrix strain per ply Differs from macroscopic strain Input for unique strain based failure criteria
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Current Status From Materials to Structure
0°
45°
90°
-45°Orientation in ply
No matrix failure in 0° ply Average matrix strain in other plies for failure of the composite
Matrix Macroscopic
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Failure Per ply definition Derived from microstructure Stress in fibers / strain in matrix
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Current Status From Materials to Structure
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Progressive Failure Analysis Explicit solver Element deletion triggered by Stress in fibers / strain in matrix
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Fiber failure
Current Status From Materials to Structure
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Progressive Failure Analysis Validation of stiffness & failure Predictive modeling
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RE on ply level of plain specimen Prediction of performance of open whole specimen
Current Status From Materials to Structure
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Progressive Failure Analysis The idea Feed the indicator, control stiffness & failure...
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Ongoing Developments From Materials to Structure
Indicator
Matrix Strain
Transverse tensile
Fibers Stress Tension
Compression
Matrix stresses & strains
Fibers stresses & strains
Composite stresses & strains
Pre-Failure
Stiffness Reduction Damage controled by failure indicator
Failure
Element Deletion Final composite failure controled by critical damage
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Progressive Failure Analysis Preliminary results 2013/02 release
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Ongoing Developments From Materials to Structure
Partial failure
No failure
Complete failure
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Progressive Failure Analysis Preliminary results 2013/02 release Stiffness degradation Failure
55
Ongoing Developments From Materials to Structure
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Deformation: d11 & d22 Element deletion: progressive & classical
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Structures
Structural Engineering
Applications
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Aerospace Industry Multi-Scale Modeling of Composite Materials & Structures
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Short Fiber Reinforcement
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Structural Engineering Structures
fibers
failure
ANISO
Measurements / curves
Process Simulation Orientation data on processing mesh
FEA Structural analysis
Structural mesh
Mapping
Anisotropic (non)linear
Material Model
ISO
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Short Fiber Reinforcement Fittings Turbine parts
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Structural Engineering Structures
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UD & Woven
59
Measurements / curves
FEA Structural analysis
Anisotropic (non)linear
Material Model
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UD
Woven
Draping Warp/weft angles
Structural Engineering Structures
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Summary
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Aerospace Industry Multi-Scale Modeling of Composite Materials & Structures
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Summary Materials
In-depth study of a broad range of materials & performances SFRP, UD & woven composites, hard metals, ceramics, nano composites Complex RVEs micro stresses & strains (Thermo-)Mechanical, thermal & electrical conductivity
From Materials to Structure
Material property evaluation Screening / Selection / Specification / Allowables
Structures Influence of processing on final performance Injection molding Draping Fiber placement ...
Aerospace Industry Multi-Scale Modeling of Composite Materials & Structures
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Digimat 4.4.1 New Release
Soon available on e-Xstream FTP! (see separate email announcement)
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Licensing sales.admin@e-Xstream.com
Support support@e-Xstream.com
Training bernard.alsteens@e-Xstream.com
Software jan.seyfarth@e-Xstream.com
Aerospace Industry Multi-Scale Modeling of Composite Materials & Structures
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Thanks a lot for your attention!
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Aerospace Industry Multi-Scale Modeling of Composite Materials & Structures