Simulation Stats

Test Case Name
tcfdcase0
Number of Points [ – ]
1
Machine Type
propeller
Rotation Speed [ RPM ]
8000.00
Number of Components [ – ]
(topology)
2
Mesh Size [ cells ]
(details)
Domain : 290349
Rotor : 217328
Total : 507677
Average y+ at walls [ – ]
(details)
Wall-clock time [ hh:mm:ss ]
00:13:03
Parallel Processors [ – ]
6
Fluid Name
air
Physical Model
incompressible
Equation of state
Numerical order
first
Turbulence model
kOmegaSST

Performance Curve

2:rotor-inlet — 2:rotor-freestream,2:rotor-outlet
Point Nr.
Advance Ratio [ – ]
Thrust Coefficient [ – ]
Torque Coefficient [ – ]
1
0.255508
0.0961792
0.0198722

Efficiency

2:rotor-inlet — 2:rotor-freestream,2:rotor-outlet
Point Nr.
Velocity Magnitude [ m/s ]
Efficiency [ – ]
1
4.32660
0.196816

Torque

Point Nr.
Torque [ N.m ]
1
0.0140063

Axial Force

Point Nr.
Axial Force [ N ]
1
0.533771

Force Coefficients

#1: 2:propeller-LETE, 2:propeller-PS, 2:propeller-SS, 2:propeller-hub
Setup Nr.
Point Nr.
Lift Coeff [ – ]
Drag Coeff [ – ]
Moment Coeff [ – ]
1
1
-0.889618
2.76083 × 10-5
0.0233438

Forces X Y Z

#1: 2:propeller-LETE, 2:propeller-PS, 2:propeller-SS, 2:propeller-hub
Setup Nr.
Point Nr.
Fx [ N ]
Fy [ N ]
Fz [ N ]
1
1
1.65650 × 10-5
-0.533771
2.46710 × 10-4

Torques X Y Z

#1: 2:propeller-LETE, 2:propeller-PS, 2:propeller-SS, 2:propeller-hub
Setup Nr.
Point Nr.
Tx [ N.m ]
Ty [ N.m ]
Tz [ N.m ]
1
1
4.53065 × 10-6
0.0140063
-3.77194 × 10-5