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Hi, this is steady-state CFD simulation report of:

eveningTest

Created by TCFD® 18.10 on Fri Oct 19 22:32:01 2018

screenshot 6
DISCOVER

Simulation Stats
Test Case Name
eveningTest
Number of Points [ – ]
1
Machine Type
propeller
Rotation Speed [ RPM ]
1145.00
Number of Components [ – ]
(topology)
2
Mesh Size [ cells ]
(details)
bounding_box : 5440267
propeller : 851732
Total : 6291999
Average y+ at walls [ – ]
(details)
392.552
Wall-clock time [ hh:mm:ss ]
01:17:21
Parallel Processors [ – ]
6
Fluid Name
air
Compressibility
incompressible
plotFlowRate 1 4
residuum 1 5

Performance Curve

1:inlet — 1:outlet
Point Nr.
Advance Ratio [ – ]
Thrust Coefficient [ – ]
Torque Coefficient [ – ]
1
1.43917
0.0181268
0.0153493
performanceCurve 1 1

Efficiency

1:inlet — 1:outlet
Point Nr.
Flow Rate [ m3/s ]
Efficiency [ – ]
1
143951.
0.270498
flowRateVsEfficiency 1 2
efficiency 1 2

Torque
Point Nr.
Torque [ N.m ]
1
2534.90
flowRateVsTorque 1 2
torque 1 2

Axial Force
Point Nr.
Axial Force [ N ]
1
913.513
flowRateVsAxialForce 1 2
axialForce 1 2

Force Coefficients

#1: 1:horizontal_stabilizer_left, 1:central_wing, 1:wing_right, 1:tail, 1:elevator_right, 1:carburetor_intake, 1:radiator_inlet_right, 1:gear_bay_left, 1:aileron_left, 1:cannon_right, 1:radiator_outlet_right, 1:rudder, 1:radiator_outlet_left, 1:wing_left, 1:gear_bay_right, 1:horizontal_stabilizer_right, 1:cannon_stub_right, 1:radiator_housing_left, 1:cannon_stub_left, 1:elevator_left, 1:carburetor_intake_housing, 1:cannon_left, 1:radiator_housing_right, 1:fuselage, 1:radiator_inlet_left, 1:canopy, 1:aileron_right, 2:blade_2, 2:blade_1, 2:blade_3, 2:hub, 2:blade_4

#2: 1:horizontal_stabilizer_left, 1:central_wing, 1:wing_right, 1:tail, 1:elevator_right, 1:carburetor_intake, 1:radiator_inlet_right, 1:gear_bay_left, 1:aileron_left, 1:cannon_right, 1:radiator_outlet_right, 1:rudder, 1:radiator_outlet_left, 1:wing_left, 1:gear_bay_right, 1:horizontal_stabilizer_right, 1:cannon_stub_right, 1:radiator_housing_left, 1:cannon_stub_left, 1:elevator_left, 1:carburetor_intake_housing, 1:cannon_left, 1:radiator_housing_right, 1:fuselage, 1:radiator_inlet_left, 1:canopy, 1:aileron_right, 2:hub

#3: 2:blade_2, 2:blade_1, 2:blade_3, 2:blade_4
Setup Nr.
Point Nr.
Lift Coeff [ – ]
Drag Coeff [ – ]
Moment Coeff [ – ]
1
1
0.360198
0.0350100
0.802156
2
1
0.356082
0.0533598
0.803587
3
1
0.00411555
-0.0183498
-0.00143072
flowRateVsForceCoeffs 1 2
forceCoeffs 1 2

Forces X Y Z

#1: 1:horizontal_stabilizer_left, 1:central_wing, 1:wing_right, 1:tail, 1:elevator_right, 1:carburetor_intake, 1:radiator_inlet_right, 1:gear_bay_left, 1:aileron_left, 1:cannon_right, 1:radiator_outlet_right, 1:rudder, 1:radiator_outlet_left, 1:wing_left, 1:gear_bay_right, 1:horizontal_stabilizer_right, 1:cannon_stub_right, 1:radiator_housing_left, 1:cannon_stub_left, 1:elevator_left, 1:carburetor_intake_housing, 1:cannon_left, 1:radiator_housing_right, 1:fuselage, 1:radiator_inlet_left, 1:canopy, 1:aileron_right, 2:blade_2, 2:blade_1, 2:blade_3, 2:hub, 2:blade_4

#2: 1:horizontal_stabilizer_left, 1:central_wing, 1:wing_right, 1:tail, 1:elevator_right, 1:carburetor_intake, 1:radiator_inlet_right, 1:gear_bay_left, 1:aileron_left, 1:cannon_right, 1:radiator_outlet_right, 1:rudder, 1:radiator_outlet_left, 1:wing_left, 1:gear_bay_right, 1:horizontal_stabilizer_right, 1:cannon_stub_right, 1:radiator_housing_left, 1:cannon_stub_left, 1:elevator_left, 1:carburetor_intake_housing, 1:cannon_left, 1:radiator_housing_right, 1:fuselage, 1:radiator_inlet_left, 1:canopy, 1:aileron_right, 2:hub

#3: 2:blade_2, 2:blade_1, 2:blade_3, 2:blade_4
Setup Nr.
Point Nr.
Fx [ N ]
Fy [ N ]
Fz [ N ]
1
1
777.040
39439.3
-2793.39
2
1
820.297
39042.3
-4809.24
3
1
-43.2571
396.997
2015.85
flowRateVsForces 1 2
forces 1 2

Torques X Y Z

#1: 1:horizontal_stabilizer_left, 1:central_wing, 1:wing_right, 1:tail, 1:elevator_right, 1:carburetor_intake, 1:radiator_inlet_right, 1:gear_bay_left, 1:aileron_left, 1:cannon_right, 1:radiator_outlet_right, 1:rudder, 1:radiator_outlet_left, 1:wing_left, 1:gear_bay_right, 1:horizontal_stabilizer_right, 1:cannon_stub_right, 1:radiator_housing_left, 1:cannon_stub_left, 1:elevator_left, 1:carburetor_intake_housing, 1:cannon_left, 1:radiator_housing_right, 1:fuselage, 1:radiator_inlet_left, 1:canopy, 1:aileron_right, 2:blade_2, 2:blade_1, 2:blade_3, 2:hub, 2:blade_4

#2: 1:horizontal_stabilizer_left, 1:central_wing, 1:wing_right, 1:tail, 1:elevator_right, 1:carburetor_intake, 1:radiator_inlet_right, 1:gear_bay_left, 1:aileron_left, 1:cannon_right, 1:radiator_outlet_right, 1:rudder, 1:radiator_outlet_left, 1:wing_left, 1:gear_bay_right, 1:horizontal_stabilizer_right, 1:cannon_stub_right, 1:radiator_housing_left, 1:cannon_stub_left, 1:elevator_left, 1:carburetor_intake_housing, 1:cannon_left, 1:radiator_housing_right, 1:fuselage, 1:radiator_inlet_left, 1:canopy, 1:aileron_right, 2:hub

#3: 2:blade_2, 2:blade_1, 2:blade_3, 2:blade_4
Setup Nr.
Point Nr.
Tx [ N.m ]
Ty [ N.m ]
Tz [ N.m ]
1
1
87637.8
-2240.60
-1858.03
2
1
87794.1
-2723.46
676.864
3
1
-156.310
482.858
-2534.90
flowRateVsMoments 1 2
moments 1 3

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