Acoustics
Perforated muffler pressure field
Adjust frequency on the fixed three-dimensional multi-chamber perforated muffler to predict the acoustic-pressure amplitude field.
AISimStudio
AI simulation case library
Explore registered simulation cases, model inputs, output fields and published verification boundaries.
Electromagnetic
Connector Signal-Integrity Vector Field
Adjust copper conductivity on the fixed three-dimensional connector geometry to predict electric- and magnetic-field magnitudes.
Thermal Stress
Thermoelastic Response of a Complex Engine Component
Adjust the hot-end temperature to predict temperature and displacement on the registered engine component body; stress is not an output.
Conjugate Heat Transfer
External air cooling of pipe components
Adjust inlet velocity and pipe conductivity to predict velocity, pressure and temperature around two pipe components with a fixed volumetric heat source; internal liquid cooling is excluded.
Compressible CFD
ONERA M6 Transonic Compressible Flow
Adjust angle of attack under the fixed Mach 0.8395 steady-Euler condition to predict eight compressible-flow fields on the ONERA M6 wing surface.
Structure
Compressor Blade Linear Static Response
Adjust total tip force on the fixed twisted compressor blade; predict SI displacement and stress with an ideal isotropic elastic material.
CFD
Parametric Darcy Flow Benchmark
Adjust permeability contrast and correlation length to view the actual input field alongside predicted 2D pressure.
CFD
Parametric Darcy Flow
Adjust permeability contrast and correlation length on a unit square with zero-pressure edges and a uniform source to view the input permeability and predicted pressure fields.
Quantum
3D Double Quantum Dot Ground State
Adjust the separation of two quantum dots in the fixed three-dimensional Gaussian-well domain to predict the ground-state wave function and probability density.
Electro-Thermo-Mechanical
Piston induction electro-thermo-mechanical coupling
Predict electromagnetic, temperature, displacement and stress fields as coil current changes at 40 kHz.
Electromagnetic-Thermal
Piston electromagnetic-thermal coupling
Predict surface electromagnetic fields and temperature as coil current changes at 40 kHz.
Electromagnetic
Complex Copper Busbar Assembly Fields
Predict signed complex E/H in registered air points around the original two complex copper DC busbar conductors from 0.1 to 0.3 GHz.
Electromagnetic
Circular Patch Panel Array Complex Fields
Predict signed complex E/H in the native array registered postprocessing cell (1,1) dielectric from 4.8 to 5.2 GHz; full-array volume and beamforming are not claimed.
Electromagnetic
Connector Complex-Field Frequency Sweep
Predict complex E/H fields and power flow from 0.10 to 5.00 GHz on a fixed connector.
Electromagnetic
Hexagonal Patch Panel Array Complex Fields
Predict signed complex E/H in the native array registered postprocessing cell (2,2) dielectric from 4.8 to 5.2 GHz; full-array volume and beamforming are not claimed.
Electromagnetic
Microwave Oven Complex Fields
Predict fixed microwave cavity and curved glass-bowl fields from 2.3 to 2.6 GHz.
Electromagnetic
MRI Birdcage Coil Complex Fields
Predict signed complex E/H in the Gel phantom loaded by the original MRI birdcage coil from 62 to 66 MHz.
Electromagnetic
Multilayer PCB Via Complex Fields
Predict signed complex E/H in the original multilayer PCB FR4 regions from 1 to 3 GHz.
Electromagnetic
SMA Edge Connector Complex Fields
Predict signed complex E/H inside the fixed official SMA connector dielectric from 1 to 3 GHz.
Electromagnetic
SMA RF Jack Complex Fields
Predict signed complex E/H inside the fixed official SMA connector dielectric from 1 to 3 GHz.
Electromagnetic
SMA Surface Mount Complex Fields
Predict signed complex E/H inside the source SMA surface-mount connector air insulation region from 1 to 3 GHz.
Fluid-Structure
Aortoiliac CMM Fluid-Structure Interaction
Adjust pulse time and peak inlet flow to predict velocity, pressure, displacement, wall shear and traction on the registered CMM wall interface.
Fluid-Structure-Thermal
ONERA M6 One-Way Aerothermoelastic Prediction
Adjust angle of attack from 2 to 4 degrees to predict flow, temperature, displacement and von Mises stress on the registered wing surface.
Multiphase CFD
MARIN 3D water-air dam break (research)
Water front impact, splash and reflected waves over 0.05–6 s. Fixed source condition; accuracy assessment failed.
Optical-Thermal
US7277232 Zoom Lens Thermal Drift
Predict lens-component temperature fields and detector optical drift across barrel temperature.
Photonics
Four-Port Silicon Microring Frequency Response
Predict full complex E/H fields and derived power flow from 1548 to 1552 nm.
Structure
PhysicsNeMo Bracket 3D Linear Elasticity
Select a downward surface traction from 20 to 60 kPa and predict 3D displacement, strain and stress on the registered bracket result mesh.
Custom PDE
2D Sparse Observation Inverse PINN
Enter observations at five fixed locations to identify coefficient a and predict the 2D scalar field, with analytic comparison for the submitted observations.
Custom PDE
2D Poisson PINN with Adjustable Boundaries
Adjust the left and right boundary values on a unit square, predict the 2D scalar field, and compare every point with the analytic solution for the submitted conditions.
Plasma MHD
SPARC Axisymmetric Plasma Equilibrium
Adjust axis pressure under the fixed 8.7 MA plasma-current and 12.2 T central-field condition to predict pressure, poloidal flux and magnetic-field components.
Structure
Ribs Elastoplastic Response
Adjust total downward end force on the fixed imported ribs mesh; predict displacement and stress in SI units.
Structure
Ribs Harmonic Response at 20 Hz
Adjust harmonic end-force amplitude at a fixed 20 Hz; predict real and imaginary displacement with mass-proportional damping alpha=2 per second.
Structure
Ribs Linear Static Response
Adjust total downward end force on the fixed imported ribs mesh; predict displacement and stress in SI units.
Structure
Ribs Geometric Nonlinear Response
Adjust total downward end force on the fixed imported ribs mesh; predict displacement and stress in SI units.
Structure
Complex Ribs Learned Buckling Prediction
Select a compressive load and buckling mode, then run the registered model to predict the three-dimensional mode shape and eigenvalue load factor.
Structure
Modal Field of a Complex Ribbed Component
Adjust Young's modulus on the fixed imported rib geometry to predict the first mode-shape field and eigenvalue.
Thermal
Transient Thermal Field of a Complex Shaft
Adjust the hot-wall and initial shaft temperatures to predict the transient temperature field of the registered complex shaft.
Structure
Cantilever Explicit Dynamics
Adjust Young's modulus and predict the end-time displacement field of a fixed three-dimensional cantilever using an explicit dynamics model.
Structure
Cantilever Implicit Dynamics
Adjust Young's modulus and predict the end-time displacement field of a fixed three-dimensional cantilever using an implicit dynamics model.
TCAD Device
3D MOSFET TCAD Field Prediction
Predict potential, electron density and hole density on a fixed 23,593-node three-dimensional MOSFET bulk mesh from gate and drain voltages.
Thermal
PCB18 Steady Thermal Prediction
Adjust the hot-boundary temperature to predict the steady temperature field on the registered PCB18 assembly sampling points.
CFD
ZPVehicle Prototype External Aerodynamics
Adjust inlet velocity from 20 to 35 m/s on the fixed ZPVehicle prototype to predict surface pressure, wall shear stress, volume velocity and pressure.