ure 2. Curvature radius conditions between the hub and blades of the propeller: (a) 4.6 mm; (b) 4.0 mm. R = 4.6 mm R = 4.0 mm Figure 2. Curvature radius conditions between the hub and blades of the propeller: (a) 4.6 mm; (b) 4.0 mm.

Published at 1233 × 406 in Development of Low-Pressure Die-Cast Al-Zn-Mg-Cu Alloy Propellers Part II: Simulations for Process Optimization

ure 2. Curvature radius conditions between the hub and blades of the propeller: (a) 4.6 mm; (b) 4.0 mm. R = 4.6 mm R = 4.0 mm Figure 2. Curvature radius conditions between the hub and blades of the propeller: (a) 4.6 mm; (b) 4.0 mm.

ure 2. Curvature radius conditions between the hub and blades of the propeller: (a) 4.6 mm; (b) 4.0 mm. R = 4.6 mm R = 4.0 mm Figure 2. Curvature radius conditions between the hub and blades of the propeller: (a) 4.6 mm; (b) 4.0 mm.

ure 2. Curvature radius conditions between the hub and blades of the propeller: (a) 4.6 mm; (b) 4.0 mm. R = 4.6 mm R = 4.0 mm Figure 2. Curvature radius conditions between the hub and blades of the propeller: (a) 4.6 mm; (b) 4.0 mm.