femap v12 nx nastran multistep nonlinear solutions · 2018-11-18 · • sol 402 multistep...
TRANSCRIPT
Femap v12
NX Nastran Multistep Nonlinear Solutions
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Agenda
Overview of NX Nastran Multistep Nonlinear Solutions
SOL 401
SOL 402
Comparison of SOL 401 vs SOL 402
Q&A
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Evolution of the NX Nastran Nonlinear Solutions
Samcef
solver
• Material Library
• Element Formulations
• Matrix Solvers
• Memory Allocation
• Output Formats
• Numerical Strategies
SOL 402
(+ environment)
Products
Solvers
Technologies
SOL 401
(+ environment)
Samcef
(+ environment)+ user interaction
Core solver engines and
associated architectures
• Components and algorithms
• Element and result consistency
• Leverage strength of each engine
NX Nastran
solver
NXN Multistep Samcef
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NX Nastran Multistep Nonlinear
SOL 401 and 402 Core Capability
• Multi-Step solutions
• Large displacement
• Plasticity
• Creep
• Contact
• Material Models
SOL 402 Difference
• Composites
• Nonlinear mechanism
SOL 401 Difference
• Multiphysics couplings
Planned
Commonalties/Differences
Multistep Solutions:
• SOL 401 and 402 provides general purpose non-linear solution capability
• SOL 401 Multistep – based on traditional NX Nastran architecture
• SOL 402 Multistep Kinematic – based on integration of Samcef in NX Nastran
Applicability
• SOL 401 and SOL 402 similarities
• Use many of the same formulations and give nearly same results
• Core set of capabilities that are the same and can be used for same applications
• Use same Nastran inputs and outputs. Easy to convert one solution to the other
SOL 401 and SOL 402 differentiations
• SOL 402 can better support nonlinear kinematic behavior
• SOL 401 can be used for multiphysics co-simulation
SOL 401
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SOL401 Multistep Solution
Support for SOL 401 added in Femap 12.0
Subcases declared Sequentially Dependent or
Not Sequentially Dependent
Contact conditions can change between Subcases
Iteration controls can change between Subcases
Analysis type can change between Subcases
• Analysis Types: Statics, Preload Bolt and Modal
are supported by Femap UI
• Subcase 1
• Analysis = Statics
• Subcase 2
• Analysis= Modal
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SOL401 NX Nastran Elements
Line Elements
• Bar
• Beam
• DOF Spring
Plane Elements
• Plate
• Laminate
• Plane Strain
Volume Elements
• Axisymmetric
• Solid
• Solid Laminate
• Solid Cohesive
0D (Other) Elements
• Spring/Damper to Ground
• DOF Spring to Ground
• Rigid
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SOL401 NX Nastran Element/Material/Solution Support
Materials Nonlinearity Solutions
Isotropic Orthotropic Anisotropic Creep
Large
Displacement Plasticity Statics Preload Modal
Bar
Beam
Plate
Laminate
Generalized
Plane Strain
Axisymmetric
Solid
Solid Laminate
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SOL401 0D, 1D Element Support
Bar and Beam Elements
• Large displacement with offsets supported
DOF Springs
• Nonlinear springs supported
• Large displacement not supported
Rigid
• RBE2, RBE3 supported
• MPCs, RBE1 NOT supported
Spring/Damper to Ground and DOF Spring to Ground
• Nonlinear Springs supported
• Large displacement not supported
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SOL401 2D Element Support
NX Nastran 12 added supported for shell elements
• Plate offsets for large displacement are supported
• CQUAD/CTRI3 automatically converted to CQUADR/CTRIAR internally
• For CQUAD8/CTRIA6 elements – K6ROT can be used to add drilling stiffness for use in curved plates
• Nonlinear Plastic and Creep shell elements –
• Allow the specification of the number of points throughout the element thickness (3, 5, 7 or 9) using the
NLAYERS parameter
• For Plastic and Creep materials, MID1, MID2, MID3 must be identical, MID4 not allowed
• Plane Strain elements CPLSTN3, CPLSTN4, CPLSTN6, CPLSTN
• Plane Stress elements CPLSTS3,CPLSTS4, CPLSTS6, CPLSTS8
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SOL401 Solid Element Support
Solid Elements
• CTETRA, CHEXA, CPENTA and CPYRA
• Axisymmetric elements CQUADX4, CQUADX8, CTRAX3, CTRAX6
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SOL 401 Cohesive Elements
Cohesive elements are used to model adhesively bonded interfaces
• Compliance in the Connection
• Damage in the material
• Two new element types: CHEXCZ and CPENTACZ
• Can occupy a solid volume or collapse to planar area
• NXN uses thickness from Property entry;
• NOT the thickness based on grid locations for the stiffness calculations
• Must reference PSOLCZ Property entry
• Material can be one of the following:
• MAT1: K01 = K02 = G / THICK, and K03S = E / THICK, where THICK is the value on the PSOLCZ bulk entry.
• MAT11: K01 = G13 / THICK, K02 = G23 / THICK, and K03S = E3 / THICK, where THICK is the value on the
PSOLCZ bulk entry
• MATCZ: Enter K01,K02,K03S on the MATCZ
• THICKness value defined for the Property is ignored
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Cohesive Elements
Cohesive elements can be created in Femap via the new meshing command
Mesh > Editing > Cohesive Meshing
• Inserts layer of solid cohesive elements
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Cohesive Material
MATCZ is used to obtain material damage estimates
• Damage estimates require material Plasticity Option
• PARAM,MATNL,1
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New concept of Connector Sets (Glue or Contact)
Similar to Nastran Reference Constraint and Load Sets
Can be used to designate Connectors used in a Master Case or Subcase
SOL 401 Contact Modeling
RMB
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SOL 401 Contact Modeling
Glue Only specified in Master Case
Contact Connections can be changed between Subcases
Master Case Boundary Conditions Sub Case Boundary Conditions
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SOL 401 Contact Connection Property
Use “Default” button to autofill most settings
New NOSEP option prevents surfaces in contact from flying
apart when the regions in contact are unloaded
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SOL 401 Glue Connection Property
Use “Default” button to autofill most settings
Sliding Glue option allows sliding but no separation
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SOL401 FEMAP support – multi-step control
Setup in the FEMAP Analysis Set Manager
Time Step and Solution Control in each Subcase
Example -
• Case 1 – ramps the structure up through a
nonlinear static case
• Case 2 – uses the stiffened results of case 1
and runs a modal solution
BC in Global
Static Case
Ramps up Force
Modal Case Seq. Dep.
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SOL401 Preview Input
Setup in the Femap Analysis Set Manager
Time step and solution control in each
subcase
Example
• Case 1 – ramps the structure up through a
nonlinear static case
• Case 2 – Uses the stiffened results of case
1 and runs a modal solution
BC in Global
Static Case
Ramps up Force
Modal Case Seq. Dep.
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SOL 401 Master and Subcase Analysis Types
Statics
Normal Modes/Eigenvalue
Bolt Preload
• Only available in a SUBCASE
Buckling
• Not supported by the Femap GUI - edit SUBCASE(s) to add a
NLARCL=AnalysisType
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SOL 401 Multistep Control Options
Control Options Can Be Changed Between Cases
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SOL 401 Multistep Nonlinear Time Steps
Mechanical and thermal loads can optionally be defined as a function of time in a static subcase
These time-assigned loads only use time as the mechanism to increment the loads.
Time Steps Are Set for Each Subcase
User Specifies the End Time,
Number of Increments and
Output Frequency
Start Time Is A Function of Case Being Sequentially Dependent or NSD
• Not Sequentially Dependent; Start Time is 0.0
• Sequentially Dependent; Start Time is End of Previous Case
Non time assigned loads can be ramped or stepped
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NX Nastran Multi-Step Nonlinear
Starting Model Case 1 – Deformed and Stiffened
Case 2 – Stiffened Model Mode 1
SOL 402
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SOL402 Nonlinear Multistep Kinematics
SOL 402 is a multi-step, structural solution that supports a combination of subcase types (static linear, static
nonlinear, nonlinear dynamic, preload, modal, Fourier, buckling) and large rotation kinematics.
SOL 402 allows a combination of the following subcases. The ANALYSIS case control command defines the
subcase analysis type with the Femap GUI
• STATICS (Nonlinear) static analysis.
• MODES Normal Modes.
• PRELOAD Bolt Preload subcase computation.
Additional Subcase types supported in NX Nastran 12 – requires manual editing of the Subcase ANALYSIS card
• DYNAMICS (Nonlinear) dynamic analysis, including damping and inertia effects.
• CYCMODES Cyclic Normal Modes.
• FOURIER Fourier Normal Modes.
• BUCKLING Buckling Modes (Incremental Stability)
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SOL402 NX Nastran Elements
Line Elements
• Bar
• Beam
• Rod
• DOF Spring
• Gap
Plane Elements
• Plate
• Laminate
• Plane Strain
Volume Elements
• Axisymmetric
• Solid
• Solid Laminate
• Solid Cohesive
0D (Other) Elements
• Mass
• Mass Matrix
• Spring/Damper to Ground
• DOF Spring to Ground
• Rigid
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SOL402 NX Nastran Element/Material/Solution Support
Materials Nonlinearity Solutions
Isotropic Orthotropic Anisotropic Creep
Large
Displacement Plasticity Statics Preload Modal
Rod
Bar
Beam
Plate
Laminate
Generalized
Plane Strain &
Plane Stress
Axisymmetric
Solid
Solid Laminate
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SOL402 1D and 0D Elements
1D Elements
• BEAM, BAR
• ROD
• GAP
0D Elements
• Springs – Linear and Nonlinear
• Dampers – Linear and Nonlinear
• RBE2, RBE3
• MASS
MPCs are also supported
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SOL402 2D (Surface) Elements
Plate Elements:
• CQUAD4,CTRIA3,CQUADR,CTRIAR,CQUAD8,CTRIA6
• CQUAD4 and CTRIA3 must be converted to CQUADR and CTRIAR in the Femap Bulk Data Form
• 2D Plane Strain
• 2D Plane Stress
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SOL402 Solid Elements
Solid Elements:
• CHEXA, CPYRAM, CTETRA, CPENTA
• 3D Axisymmetric elements: CTRAX3, CTRAX6, CTRIAX, CQUADX4,
CQUADX8, CQUADX
• Solid Cohesive elements: CHEXCZ, CPENTCZ
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SOL 402 Hyperelastic Materials
Three (3) Hyperelastic material types available
• Mooney-Rivlin
• Hyperfoam
• Ogden
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SOL 402 Contact Modeling
Solid and Beam Bolted Connections
Rigid Connection Regions
Glued or Contact Connector Sets, similar to Nastran Reference Constraint and Load Sets can be used to
designate Connectors used in a Master or Subcase
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SOL 402 Contact and Glued Connection Properties
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SOL 402 Analysis Set
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SOL 402 Analysis Type and Control Options
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SOL 402 Multistep Nonlinear Time Steps
Mechanical and thermal loads can optionally be defined as a function of time in a static subcase.
These time-assigned loads only use time as the mechanism to increment the loads.
• Time Steps Are Set for Each Subcase
• User Specifies the End Time, Number of Increments, Output Frequency
• Start Time Is A Function of Case Being Sequentially Dependent or NSD
• Not Sequentially Dependent; Start Time is 0.0
• Sequentially Dependent; Start Time is End of Previous Case
• Non Time Assigned Loads Can be Ramped or Stepped
SOL 401 vs 402
Comparison
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SOL 402 vs SOL 401 Comparison
General
• SOL 401 can be used for multiphysics co-simulation
• SOL 402 should be used to simulate nonlinear kinematic behavior
Contact
• In SOL 401, the OFFSET distance can be defined per contact region (BCRPARA bulk entry)
• In SOL 402, the OFFSET distance is defined at the contact level (BCTPAR2 entry).
• In SOL 401, a contact with shells automatically take the half thicknesses of the shells into account.
• In SOL 402, must manually take the half thicknesses of the shells into account with the OFFSET parameter
for the Connection Property used for that Connection
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SOL 402 vs SOL 401 Bolt Comparison
SOL 401
• Bolts can only modeled with solid elements
• You also cannot use CPYRAM and/or composite solids for a BOLT of the ETYPE=3 type.
• Bolt loading sequence (BOLTSEQ) is allowed in SOL 401
• Initial strain bolt preload force is allowed in SOL 40I
SOL 402
• Bolts can be modeled using beams and solid elements
• Bolts are activated for the whole subcase time interval.
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SOL 402 vs SOL 401 SUBCASE Comparison
In SOL 401, a NSD subcase (SEQDEP = NO) has a start time of zero. In addition, a non-sequentially
dependent static or modal subcase does not use the displacement/stress/strain state from the previous
static subcase.
In SOL 402, a NSD subcase uses the final time from the previous subcase for its start time. But the
computation state (stresses, state variables, and so on) can be reloaded from the end of any of the
previous subcases through the RSUB parameter of the NLCNTL2 bulk entry.
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Multistep Nonlinear Documents
SOL 401 - Multi-Step Nonlinear User’s Guide: multi_step_nonlinear.pdf
SOL 402 – NX Nastran 12 Release Guide, Chapter 6: release_guide.pdf
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Q&A
Backup
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SOL 402 Multi-Step Global Strategy Control Options