Services
Aerodynamic Analysis & CFD
Computational fluid dynamics for lift, drag and stability questions — with the mesh study and validation that make the numbers worth quoting.
A CFD result is only as good as the assumptions behind it, so those are stated up front: domain size, turbulence model, boundary conditions and what the study can and cannot resolve. Mesh independence is demonstrated rather than claimed, and results are compared against analytical estimates, wind tunnel data or published cases wherever a reference exists.
Suited to aerofoil and wing performance, propeller and rotor characterisation, external flow over vehicles and structures, cooling and ventilation studies, and configuration trade-offs during early design.
How the work runs
Define the question and the accuracy it deserves → geometry preparation → meshing with an independence study → solver setup → validation against a reference → reporting with assumptions and limitations stated.