From engineering question to defensible design decision.
ANSYS Fluent · OpenFOAM · Python · AI / ML
From an early configuration to a defensible design decision, each engagement is scoped around the question you need answered.
Drag polars, pressure and velocity fields, transition, stability, propeller and duct flow, thermal analysis and combustion — ANSYS Fluent and OpenFOAM.
Airframe shaping, drag reduction, propeller analysis and motor–propeller–battery matching for VTOL, tail-sitter and fixed-wing UAVs.
Design of experiments, surrogate models, test correlation, automated post-processing and trade studies for faster, evidence-based iteration.
A closed-loop conceptual design process — sizing, aerodynamic and propulsion analysis, dynamics and control, iterated to convergence.
Representative high-fidelity CFD — streamlines, pressure and velocity fields used to cut drag, size propulsion and verify stability.
A live, interactive workbench — no signup. Size and analyze the vehicle, then take it to full-fidelity CFD and optimization.
Get a focused recommendation on the most efficient analysis path and the outputs needed to move the design forward.
Discuss your project