FLOW STUDIES 01 / AERODYNAMICS
Illustrative finite-wing estimate. 1 m chord × 4 m span. α −4° to 10°; attached, incompressible flow. Fixed Cᴅ₀ = 0.012; e = 0.8; ρ = 1.225 kg/m³. No stall or turbulence model.
Sample output · fictional lab Flow paths are illustrative, not CFD.