Paraglider Wing-Loading, High-Altitude Takeoff TAS & MacCready Speed-Bar Polar Solver

Deterministic ISA non-standard density altitude TAS = IAS * sqrt(rho_0 / rho_alt) + Reichmann MacCready speed-to-fly tangent on quadratic paraglider sink polar engine (.json, .igc, .csv, .pdf) built for Ozone Paragliders, Advance, Nova, Gin Gliders — zero-upload ephemeral Wasm RAM execution.

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