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Automation components for simulation-based engineering. simulation-based engineering challenges. Use of physics simulation as an integral part of the design process Use of simulation early and often in the design process Use of simulation to evaluate design functional objectives
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simulation-based engineeringchallenges • Use of physics simulation as an integral part of the design process • Use of simulation early and often in the design process • Use of simulation to evaluate design functional objectives • Use of simulation to affect design decisions
simulation-based engineeringchallenges • Increasing complexity • Structural Analysis • Thermal Analysis • Computational Fluid Dynamics (CFD) • ElectroMagnetic Analysis • Radiation Analysis • Coupled Physics • MEMS • Application specific • Turbo-machinery • Power generation • Combustion engines • Chemical Mixing • . . .
simulation-based engineeringchallenges • objectives of physics simulation in the design process are changing • Drive reusable Analysis Data Models from high level requirements through detailed analysis. • Concept to detail design phases • Provide a means to support robust design, systems engineering, functional design and design space exploration for performance investigations. • Provide Analysis data definition to enable capture and reuse of expertise.
simulation-based engineering environment Simulation Driver Frameworks (Robust Design / Design Exploration / Systems Engineering) Instance-Independent Simulation Definition (Analysis Abstract Model) Simulation Results Instance Data Simulation Execution Instance Model Simulation Instance Model Solve for Frameworks Data Management Frameworks (PLM/SDM) Rules, Processes, Templates Instance Based Simulation Data (Execution Ready/Results Data) Simulation Models Object Definition Instance Data (CAD, Mesh Based, Concept, Non-Geometric)
Simmetrix approach • Provide software components to enable automation to generate accurate simulation results applicable to design decisions directly from the current Design Model instance on a repetitive basis through the design process • Abstract Model • Simulation Model • Direct geometry access • Automatic mesh generation • Automatic generation of run-ready data • Results management • Adaptive mesh modification
analysis abstract model • Instance Independent Simulation Definition Made up of Four Major Aspects Physical Characteristics Instantiation Rules and Processes Solution Specific Definitions Conceptual Model
analysis abstract model • Instance Independent Simulation Definition • Physical characteristics • Physical constraints and properties that are instance independent • Material definitions/libraries • Physical constraints • others • Defined / utilized as attributes assigned to a global / nothing Class in the Conceptual Model
analysis abstract model • Instance Independent Simulation Definition • Solution Specific Definitions • Definitions of the specific problem to be solved • Defined as attributes assigned to data objects (or global class) in the conceptual model • Can be expanded to include definition of derived results (Performance Requirements) calculation
analysis abstract model • Abstract (Conceptual) Model • Tag based approach • Tags placed on our associated with Object Definition Data • Typically string parameters or attributes • Tags can be assigned to Assemblies, subassemblies, parts, features, and explicit Faces • Auxiliary file used for Discrete (mesh) data • Benefits • Independent of complexity of problem domain • Can work with object definitions from multiple sources • Limitations & Issues • Requires creation and maintenance of persistent tag data • Difficult to maintain tags at anything less than a feature • (ie a-pillar flange ) • Applicable to a limited domain of problems
analysis abstract model • Abstract (Conceptual) Model • Tag based approach • Simple Heat Exchanger example • CFD simulation defined once and alternate designs instanced • first design could be in CAD system A and second design in CAD system B • Boundary Layer meshing and wall boundary conditions applied to all appropriate faces
analysis abstract model • Abstract (Conceptual) Model • Abstract Reasoning based approach • Abstract Geometry • Component Functions & Filters • Result in Component / Abstract Geometry • Can be used to drive complex “rule” like structure (ie matching edge loop pairs for pin or bolt hole locations) • Operations on Components / Abstract Geometry • Relations, Groups, Functions & Filters • Result in Component / Abstract Geometry • Can be nested to form complex abstract objects • Benefits • Independent of object data structure (ie CAD features) • Removes need for tags • Can work with object definitions from multiple sources • Applicable to a broad domain of problems • Limitations & Issues • Complexity of problem domain determines complexity of Abstract Reasoning
analysis abstract model • Abstract (Conceptual) Model • Abstract Reasoning based approach • Decklid example • Decklid analysis starting with existing NASTRAN mesh models • Loads & boundary conditions defined abstractly and located based on each instance
analysis abstract model • Abstract (Conceptual) Model • Mixed approach • Abstract Reasoning + Tags • Best of both worlds approach • Benefits • Leverages knowledge that is available • Minimizes need for tags to what is easy & appropriate to tag • Reduces complexity of Abstract Reasoning by only using Abstract Reasoning where tags are not appropriate • Independent of object data structure (ie CAD features) • Removes need for tags • Can work with object definitions from multiple sources • Applicable to complete domain of problems • Limitations & Issues • Requires planning when & what tags are appropriate • Yet another layer of abstraction
analysis abstract model • Instance Independent Simulation Definition • Instantiation Rules and Processes • Transformation mappings from various object definition instance representation types to valid simulation instance models (implicit). • Includes instantiation of relations data • Includes instantiation of derived data • inverse space for CFD/EM • “sliver” feature removal • Different for each object definition instance representation type • Included as part of GeomSim modules for supported object definition representation types
simulation model • The Object Definition Instance (“Design Model”) is transformed into a non-manifold topology (Simulation Model) • Solids that touch share common faces and edges at the contact interface • Resulting interface faces may have material on both sides • Allows for single or set of mesh entities at the interface • Attributes may be used to create duplicate mesh entities at the interface • Attributes are recast from the Abstract Model to the Simulation Model for the current Design Model instance
simulation model • A Unified Topology Model is created independent of geometry source (also works with discrete models – stl/mesh models) • Initially generated from Design Model instance • Provides interrogations of geometry via direct access of the Design Model • Topological adjacencies, point classification, surface evaluation (points, derivatives, normals, etc.), closest point queries, etc. • Assembly modeling • Represent assembly models as non-manifold model even if the underlying modeling engine does not support this • Allows for creation and modification of simulation related topology • Suppression of “small” features • Addition of bounding boxes • Symmetry planes • Recognition of void regions that are not explicitly defined in the modeling source • Simulation Model topology does not have to exactly match the Design Model topology
automatic mesh generation • Mesh control attributes assigned to the Abstract Model are mapped to the appropriate entities in the current Simulation Model instance. • Supports non-manifold topology models • embedded vertices, edges, faces • Maintains relationship of mesh entities to Simulation Model topology • Provides ability to put a full or partial mesh on a model entity
Courtesy Top Systems Ltd Courtesy Ford Motor Company Courtesy Infolytica Corporation automatic mesh generation • Fully automatic mesh generation for surfaces and solids • Triangular, quadrilateral and mixed surface meshes • Tetrahedral volume meshes
Courtesy Top Systems Ltd. automatic mesh generation • Curved mesh generation • Supports meshes of higher order elements that capture geometry
Courtesy Infolytica Corporation automatic mesh generation • Matched meshes for periodic boundary conditions
automatic mesh generation • Boundary Layer meshing with edge blends
automatic mesh generation • Extrusion meshing • Extrude mesh between two faces with similar topology • Supports generalized curvature between faces
automatic mesh generation • Crack Tip meshing • 3D edge blends along crack tip edge
automatic mesh generation • Extensive mesh refinement control • Specified refinement size • Absolute value on model, model entity or location in space • Relative value on model or model entity • Function based on location in space • Boundary layer growth rate • Curvature based mesh refinement • User defined refinement
A unified representation of simulation results data that is independent of the physics solver used • Provide result feedback in terms of design objectives and criteria • Provide improved data for visualization software • Provide high level access and query functions
results management • Expressions • Are based on operations on one or more fields • Can be created from multiple fields • Fields may be on the same or different meshes • Can create new fields • Can store what the field represents • Can be evaluated over any part of the domain • Can be evaluated over Components or Classes in the Abstract Model • Can be used to express results in terms of design objectives (e.g. comfort index, bearing force, power drop, …)
results management • Supports mapping solutions between meshes • Different physics • Same physics but different mesh • Adaptive mesh modification • Solution migration during repartitioning
adaptive mesh modification • Provides refinement and coarsening of existing mesh • Ensures new nodes on boundary are placed correctly on geometry and mesh is valid • Enables anisotropic target mesh
geometry based parallel mesh generation & adaptivity • Growing need to solve larger and larger problems • Fluid domain applications (automotive & aerospace) • Biomedical applications • Environmental applications • Electromagnetic applications • Coupled applications
geometry based parallel mesh generation & adaptivity • Growing need to solve larger and larger problems • Tens of millions of elements are becoming prevalent • Hundreds of millions of elements are becoming common • Applications requiring billions of elements are appearing
geometry based parallel mesh generation & adaptivity • Solvers have made significant advances in parallelization • Parallel CFD and EM solves are quite common • Recent advances have shown excellent scaling results on large paralleled clusters (ref. Ken Jansen) • Meshing Technology has not kept up with solver technology in the area of Parallel computing • Some advances have been made in Parallel mesh adaptation • Some work has been done in Parallel mesh generation • A few applications have Distributed memory parallel meshing available • A few more applications have Shared memory parallel meshing available • Most applications start the parallel meshing with an initial facetted model • Mesh generation for the large scale problems is clearly becoming the bottleneck
geometry based parallel mesh generation & adaptivity • Parallel mesh generation brings with it its own set of problems / issues • For generalized meshing of arbitrary geometry the problem is ill formed for parallel computing • An added complexity is that the intent for CFD, EM and other far-field applications is to model the space defining the field volume with one or more complex volumes • Just splitting the workload by parts in an assembly is not appropriate
geometry based parallel mesh generation & adaptivity • Accurate solutions require accurate capture of geometry • Curvature based refinement is commonly used in serial mesh generation applications • Small details may be of interest • Using a predefined facet model may not be accurate enough for the critical areas of interest • Accurate capture of geometry requires direct geometry access as part of the parallel mesh generation • Creating a highly accurate facet model is a serial operation and would quickly become the new bottleneck
geometry based parallel mesh generation & adaptivity • Shared Memory .vs. Distributed Memory • 64 bit processors and multi-core systems have raised the question of Shared Memory (multi-threaded) or Distributed Memory (MPI) architectures • The answer is basically related to the size of mesh required • The limitation on Shared Memory Parallel has moved from the addressable memory space to the amount of physical memory available • The main issue with Distributed Memory Parallel is to get enough regions to be meshed on each processor to avoid a negative impact from communications • Three groupings of problems can be considered • Moderately large – (millions to low tens of millions of elements) – SMP • Large – (low tens of millions to high tens of millions) – either • Very Large – (> high tens of millions) - DMP • Simmetrix has developed a set of toolkits for Geometry Based Parallel Mesh generation for both SMP and DMP architectures
geometry based parallel mesh generation & adaptivity • A series of rooms with furniture and people (Parasolid model) • (courtesy of Transpire , Inc.) • Walls, Furniture, people and space are meshed • With BL for CFD type applications • Without BL for EM type applications • Results shown for various configurations of Distributed Memory Parallel (DMP) on a small cluster
geometry based parallel mesh generation & adaptivity • Cluster configuration used for testing (low end cluster) • 6 dual core Suns • 2Ghz Opteron processors • 2GB Ram per processor • Gigabit Ethernet connection • Speedup Test • 3 different mesh sizes run with and without Boundary Layers • ~ 6 Million mesh regions run on 2, 4, and 8 processors • ~ 24 Million mesh regions run on 4 and 8 processors • ~ 46 Million mesh regions run on 4, 6, 8,10 and 12 processors • Normalized Speedup = ( t(b) * n(b) ) / ( t(n) * n ) • t(b) – meshing time for base (minimum number of processors run) • n(b) – number of base processors • t(n) – meshing time for n processors • n – number of processors used
geometry based parallel mesh generation & adaptivity • 6 million mesh regions • ~1.5 million mesh regions/minute on 2 processors • ~2.3 million mesh regions/minute on 4 processors • ~3.6 million mesh regions/minute on 8 processors
geometry based parallel mesh generation & adaptivity • 6 Million mesh regions
geometry based parallel mesh generation & adaptivity • 24 million mesh regions • ~ 3 Million mesh regions/minute on 4 processors • ~ 4.3 Million mesh regions/minute on 8 processors
geometry based parallel mesh generation & adaptivity • 24 Million mesh regions
geometry based parallel mesh generation & adaptivity • 46 million mesh regions • ~ 2.7 Million mesh regions/minute on 4 processors • ~ 3 Million mesh regions/minute on 6 processors • ~ 3.5 Million mesh regions/minute on 8 processors • ~ 4.9 Million mesh regions/minute on 10 processors • ~ 5.3 Million mesh regions/minute on 10 processors
geometry based parallel mesh generation & adaptivity • 6 Million mesh regions – normalized speedup
geometry based parallel mesh generation & adaptivity • Parallel Mesh adaptivity • Supports isotropic and anisotropic mesh adaptivity • Supports refinement & coarsening • Adapted mesh adheres to original geometry • Supports initial mesh as partitioned or single mesh