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Propeller Performance: UIUC DA4002 D18 P10

0.5 to 0.9

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.

Mechanical Engineeringpropeller key: UIUC DA4002 D18 P109 rowsPage 2 of 2
propeller keyadvance ratio JRPM 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 familythrust coefficient CT (dimensionless)
UIUC DA4002 D18 P100.54,000197,000180.68612100.55560.0454UIUC DA40020.0623
UIUC DA4002 D18 P100.554,000197,000180.70299100.55560.0435UIUC DA40020.0556
UIUC DA4002 D18 P100.64,000197,000180.70315100.55560.0413UIUC DA40020.0484
UIUC DA4002 D18 P100.654,000197,000180.68527100.55560.0387UIUC DA40020.0408
UIUC DA4002 D18 P100.74,000197,000180.63922100.55560.0357UIUC DA40020.0326
UIUC DA4002 D18 P100.754,000197,000180.55495100.55560.0323UIUC DA40020.0239
UIUC DA4002 D18 P100.84,000197,000180.41544100.55560.0285UIUC DA40020.0148
UIUC DA4002 D18 P100.854,000197,000180.1749100.55560.0243UIUC DA40020.005
UIUC DA4002 D18 P100.94,000197,000180100.55560.0195UIUC DA40020

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