Simulation Stats

Test Case Name
propeller-DJI-9450-6M
Number of Points [ – ]
1
Machine Type
propeller
Rotation Speed [ RPM ]
6000.00
Number of Components [ – ]
(topology)
2
Mesh Size [ cells ]
(details)
Domain : 2728258
Rotor : 3698258
Total : 6426516
Average y+ at walls [ – ]
details
Wall-clock time [ hh:mm:ss ]
00:05:34 (meshing)
38:35:29 (calculation)
Parallel Processors [ – ]
24
Fluid Name
air
Physical Model
compressible
Numerical order
second
Turbulence model
kOmegaSST

Performance Curve

2:rotor-inlet — 2:rotor-freestream,2:rotor-outlet
Point Nr.
Advance Ratio [ – ]
Thrust Coefficient [ – ]
Torque Coefficient [ – ]
1
0.284402
0.0862920
0.00605732

Efficiency

2:rotor-inlet — 2:rotor-freestream,2:rotor-outlet
Point Nr.
Flow Rate [ kg/s ]
Efficiency [ – ]
1
0.255076
0.644826

Torque

Point Nr.
Torque [ N.m ]
1
0.0579163

Axial Force

Point Nr.
Axial Force [ N ]
1
3.43779

Radial Force

Point Nr.
Radial Force [ N ]
1
0.0225298

Power

Point Nr.
Power [ W ]
1
36.3899

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
1.18691 × 10-4
-1.12928 × 10-4
-5.09178 × 10-5

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
-6.77569 × 10-5
7.12144 × 10-5
-3.43779

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
7.78638 × 10-5
-3.05507 × 10-5
0.0579163