UAV Design, Simulation & CFD, Data Analysis & Optimization
From engineering question to defensible design decision.
ANSYS Fluent · OpenFOAM · Python · AI / ML
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.
Free, physics-based sizing tools that run live, right here in the browser — no signup.
Define a hover + cruise mission and size the pack: thrust → power → energy → capacity → weight, plus energy- vs current-limited checks.
Size diameter and pitch from your target speed, available thrust and motor RPM, with pitch-speed and tip-Mach feasibility checks.
More calculators (wing loading, trim & stability, stall & AoA…) are being converted natively one at a time. Until then, the full suite is available in the external app.
Get a focused recommendation on the most efficient analysis path and the outputs needed to move the design forward.
Discuss your project