Propeller Performance: UIUC_DA4002_D18_P10
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) |
|---|---|---|---|---|---|---|---|---|---|---|
| UIUC_DA4002_D18_P10 | 0 | 4,000 | 197,000 | 18 | 0 | 10 | 0.5556 | 0.049 | UIUC_DA4002 | 0.105 |
| UIUC_DA4002_D18_P10 | 0.05 | 4,000 | 197,000 | 18 | 0.10354 | 10 | 0.5556 | 0.0495 | UIUC_DA4002 | 0.1025 |
| UIUC_DA4002_D18_P10 | 0.1 | 4,000 | 197,000 | 18 | 0.1996 | 10 | 0.5556 | 0.0499 | UIUC_DA4002 | 0.0996 |
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