RC Thermal & Slope Glider Low-Reynolds Polar & MacCready Wing-Ballast Solver

Deterministic Low-Reynolds XFOIL-fitted drag polar scaling (Cd ~ Re^-0.5) + classic MacCready optimal inter-thermal airspeed tangent equation engine (.dat, .pol, .csv, .json) built for Vladimir's Model, Aer-O-Tec, Jeti Duplex, FrSky — zero-upload ephemeral Wasm RAM execution.

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Cloudflare Ephemeral Wasm RAM · 0% Retention

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