Fixed-Wing RC & UAV Neutral Point, Static Margin (% MAC) & Stall Speed Solver

Deterministic Vortex-Lattice simplified Prandtl/Panknin swept-wing aerodynamic center formula + tail volume coefficient V_h neutral-point shift engine (.json, .csv, .dxf) built for Sonicmodell, AtomRC, HeeWing, Multiplex — zero-upload ephemeral Wasm RAM execution.

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Cloudflare Ephemeral Wasm RAM · 0% Retention

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