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TECHNICAL APPROACH PROPELLER
TECHNICAL APPROACH NACELLE
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0.8 Mach number advance ratio aerodynamic modeling features airfoil characteristics analysis angle of attack application Area Ruled Spinner axial axisymmetric Biot-Savart Law blade angle blade element coordinate blade forces blade pitch blade row boundary layer cartesian coordinate system cascade correlation cascade data chordwise CM CM CM conical flow cylindrical coordinate system drag coefficient effect element coordinate system equations flow field high speed propeller induced velocity inflow influence isolated airfoil data lift coefficient lifting line linear m m m m m Mach number condition modeling option NACA nacelle NASA normalwise o o o o o o obtained performance predictions potential flow power coefficient predicted efficiencies propeller blade propeller designs propeller efficiency propeller performance propeller-nacelle reference spanwise SR-3 propeller streamline curvature test data test results tip loss models unit vector viscous vortex wake geometry YES TIP LOSS