Solving complex transonic challenges through high-fidelity Fluid-Structure Interaction (FSI). We bridge the gap between theoretical flight physics and structural failure through predictive simulation.
Explore Aero PortfolioAdvanced pressure field mapping and shock-wave boundary analysis for Mach 0.8 to 1.2 flight regimes.
Identifying and mitigating catastrophic structural resonance in aerodynamic components through modal coupling.
Real-time coupling of fluid flow and structural deformation to simulate real-world environmental stress.
| Analysis Type | Software Stack | Validation Method |
|---|---|---|
| Transient CFD | Ansys Fluent / CFX | Grid Convergence Study |
| Aero-Elasticity | Matlab / Ansys Mechanical | Modal Coupling Verification |
| Turbulence Modeling | K-Omega SST | Experimental Data Matching |
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projects@mechdynlab.com
London, United Kingdom