Deterministic Blended aerodynamic lift (0.5*rho*V_IAS^2*S*C_L(alpha)) + vertical rotor thrust continuity envelope across transition airspeed ramp engine (.bin, .log, .param) built for ArduPlane VTOL, CUAV, Foxtech, Quantum-Systems — zero-upload ephemeral Wasm RAM execution.
Running ephemeral Wasm verification…