Propeller Performance: APC_thin_electric_D12_P6
Propeller thrust coefficient (CT), power coefficient (CP), and propulsive efficiency (eta) versus advance ratio J for standard propeller families: APC sport, APC thin electric, NACA Clark Y general aviation, UIUC DA4002 benchmark, and generic variable-pitch. Covers UAV/hobby propellers (8–18 inch) and general aviation (72–74 inch). Data sourced from APC published performance files, UIUC Propeller Database (Brandt & Selig), and NACA Report 640.
| propeller key | advance ratio J | RPM reference (rpm) | Reynolds number reference (dimensionless) | diameter in (in) | efficiency eta (dimensionless) | pitch in (in) | pitch to diameter ratio (dimensionless) | power coefficient CP (dimensionless) | propeller family | thrust coefficient CT (dimensionless) |
|---|---|---|---|---|---|---|---|---|---|---|
| APC_thin_electric_D12_P6 | 0 | 5,000 | 109,000 | 12 | 0 | 6 | 0.5 | 0.0373 | APC_thin_electric | 0.1003 |
| APC_thin_electric_D12_P6 | 0.05 | 5,000 | 109,000 | 12 | 0.12857 | 6 | 0.5 | 0.0378 | APC_thin_electric | 0.0972 |
| APC_thin_electric_D12_P6 | 0.1 | 5,000 | 109,000 | 12 | 0.24541 | 6 | 0.5 | 0.0381 | APC_thin_electric | 0.0935 |
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