Fluid-Structure Interaction

Tightly coupled FSI, the intelligent way


Developed specifically to work seamlessly with CFD++® and CSM++®, MetaFSI® is Metacomp’s suite of tools that enable two-way tightly-coupled Fluid-Thermal-Structural Interaction (FTSI) simulations.

OVERVIEW

What is MetaFSI®?

FSI, the intelligent way

MetaFSI is a suite of tools that provides the easiest way to integrate a tightly coupled fluid-thermal-structure interaction with CFD++® and CSM++®. MetaFSI® primarily handles transfer of fluid loads from CFD mesh boundaries and applies them on a topologically dissimilar structural mesh while preserving total load. MetaFSI® is also responsible for morphing the CFD++® mesh based on the received CSM++® solution, using a robust mesh morphing algorithm that has been developed and evolved using real-world test cases.

Easy-to-use, easy-to-learn

Experience a different level of ease-of-use and productivity with the Advanced User Interface that is shared with CSM++®. The MetaFSI® interface is automatically presented from within the same CSM++® Advanced User Interface when an FSI analysis option is chosen during setup. And since MetaFSI® is also based upon our ICMP (Integral Computational Multi-Physics) framework underpinning both CSM++® and CFD++®, it offers a tightly coupled FSI setup process with an easy and consistent user experience across the entire FSI simulation procedure.


FEATURES

MetaFSI® performs these two key functions to enable tight-coupling between CFD++® and CSM++®

Load & Displacement Transfer

  • Gathers loads from CFD++® boundaries
    • Surface pressures and wall shears
    • Heat fluxes and surface temperatures
  • Applies to chosen CSM++® boundaries
    • Mechanical loads, applied as forces and moments
    • Thermal loads, applied as heat fluxes, convective and radiative loads
  • Handles the transfer in a way that preservers total load and center of pressure
  • Transfers computed CSM++® solution back to CFD++® boundaries using nearest-neighbor interpolation

Mesh Morphing

  • Morphs CFD++® mesh based on computed CSM++® solution
    • Retains same mesh topology as original mesh
    • Morphs either the entire mesh or limits to a user-defined region
  • Propagates transferred deformations at boundaries into the volume
    • Computes a 3-D interpolating function using radial-basis-functions
    • Calculates updated nodal locations using interpolant
    • Uses multi-process parallelism to speed up the morphing process
  • Provides users fine-grain control over the morphing procedure

MetaFSI® contains a plethora of features that make it possible to tailor the coupling algorithm to your needs

Implicit and explicit coupling strategies
Two-way and one-way coupling
Normal modes based coupling
Coupling between 3-D CFD boundaries and 1D/2D CSM boundaries
Separate thermal and structural models for FTSI
MPI-based communication between MetaFSI®, CFD++® and CSM++®
Control point coarsening and augmentation
Displacement relaxation
Morphing tests before job submission

… and several other advanced features! See the MetaFSI® Product Overview for additional details

See MetaFSI in action

Product Overview

APPLICATIONS
Turek-Hron FSI2 Benchmark – Cylinder with flag
Time history of lift and drag on cylinder + flag assembly
Time history of x and Y displacements
Static FSI of the NASA Common Research Model
Bending deformation along wingspan
Twisting deformation along wingspan
Flutter analysis of the highly flexible “Pazy” wing

Nonlinear static equilibrium state, about which a linear flutter analysis is performed using deformed normal modes

Predicted stability boundary at a range of flutter speeds

Flutter analysis of the Pazy wing (3rd AIAA Aeroelasticity Prediction Workshop)

Time history of tip twist as the wing goes unstable

Fluid-thermal-Structural interaction of a missile configuration

CFD++® analysis of a missile at Mach 5 (top), with the corresponding CSM++® structural (middle, coarser mesh) and thermal (bottom, finer mesh) models

Temperature contours over time, shown over an exaggerated deformation of missile geometry