Propeller Thrust Calculator
Calculate static and dynamic thrust for propellers using momentum actuator disk theory. Supports air and water mediums with empirical thrust coefficients.
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Applications
Estimate static and dynamic thrust for aircraft, drone, and marine propellers. Used by drone builders for motor-propeller matching, RC hobbyists for performance prediction, aerospace students for education, and marine engineers for propulsion system design.
Calculation Methodology
Uses momentum actuator disk theory with empirical thrust coefficient (Ct ≈ 0.105 for typical RC props). Static thrust: T = Ct × ρ × n² × D⁴. Dynamic thrust solves actuator disk equations iteratively. Air density uses ISA model for altitude correction. Water density (fresh: 999.1, salt: 1025.0 kg/m³). Ct adjusted by blade count and pitch/diameter ratio.
Fun Fact: The actuator disk model was developed by Rankine (1865) and Froude (1889) — over 160 years old and still the standard model for propeller and helicopter rotor analysis! A 10-inch drone propeller at 10,000 RPM generates enough thrust to lift about 250 kg — if you scaled it up to a 5-meter diameter at the same RPM, it could lift a small house.
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