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

Axial-Fan-Stage

Created by TCFD 21.02 on Mon Feb 22 14:28:22 2021

screenshot 4

Simulation Stats

Test Case Name
Axial-Fan-Stage
Number of Points [ – ]
5
Machine Type
fan
Rotation Speed [ RPM ]
3000.00
Number of Components [ – ]
( topology )
2
Mesh Size [ cells ]
( details )
rotor : 285261
stator : 301333
Total : 586594
Simulation score [ – ]
details
Average y+ at walls [ – ]
details
Wall-clock time [ hh:mm:ss ]
00:00:37 (meshing)
00:20:03 (calculation)
Parallel Processors [ – ]
24
Fluid Name
air
Physical Model
incompressible
Numerical order
second
Turbulence model
kOmegaSST
plotFlowRate 1 2
residuum 1 1

Fan Characteristic

Point Nr.
Flow number [ – ]
Compression number [ – ]
1
0.486020
0.378417
2
0.423021
0.506943
3
0.371839
0.584928
4
0.324313
0.634780
5
0.292528
0.642781
compression 1

Efficiency

1:rotor-inlet — 2:stator-outlet

Point Nr.
Flow Rate [ m3/s ]
Efficiency [ – ]
1
7.49939
0.800447
2
6.52730
0.872377
3
5.73755
0.881600
4
5.00422
0.866991
5
4.51377
0.839905
flowRateVsEfficiency 1 1
efficiency 1 1

Torque

Point Nr.
Torque [ N.m ]
1
41.5740
2
44.4031
3
44.5214
4
42.8308
5
40.3810
flowRateVsTorque 1 1
torque 1 1

Axial Force

Point Nr.
Axial Force [ N ]
1
-192.569
2
-245.547
3
-274.348
4
-292.062
5
-293.255
flowRateVsAxialForce 1 1
axialForce 1 1

Radial Force

Point Nr.
Radial Force [ N ]
1
21469.9
2
21562.4
3
21620.6
4
21663.8
5
21684.9
flowRateVsRadialForce 1 1
radialForce 1 1

Total Pressure Difference

1:rotor-inlet — 2:stator-outlet

Point Nr.
Flow Rate [ m3/s ]
Total Pressure Difference [ Pa ]
1
7.49939
1400.56
2
6.52730
1876.24
3
5.73755
2164.87
4
5.00422
2349.38
5
4.51377
2378.99
flowRateVsTotalPressureDifference 1 1
totalPressureDifference 1 1

Total Pressure per Interfaces

Point Nr.
Interface Name
Flow Rate [ m3/s ]
Total Pressure [ Pa ]
1
rotor-in
7.49939
101325.
1
rotor-to-stator
7.49875
102839.
1
stator-from-rotor
7.49877
102814.
1
stator-out
7.49900
102726.
2
rotor-in
6.52730
101325.
2
rotor-to-stator
6.52654
103312.
2
stator-from-rotor
6.52655
103290.
2
stator-out
6.52679
103201.
3
rotor-in
5.73755
101325.
3
rotor-to-stator
5.73652
103624.
3
stator-from-rotor
5.73655
103599.
3
stator-out
5.73631
103490.
4
rotor-in
5.00422
101325.
4
rotor-to-stator
5.00291
103855.
4
stator-from-rotor
5.00291
103830.
4
stator-out
5.00243
103674.
5
rotor-in
4.51377
101325.
5
rotor-to-stator
4.51200
103924.
5
stator-from-rotor
4.51200
103886.
5
stator-out
4.51158
103704.
flowRateVsTotalPressurePerInterfaces rotor in 1
totalPressurePerInterfaces rotor in 1
totalPressureProfile 1 2

Velocity Magnitude per Interfaces

Point Nr.
Interface Name
Flow Rate [ m3/s ]
Velocity Magnitude [ m/s ]
1
rotor-in
7.49939
47.3640
1
rotor-to-stator
7.49875
52.7666
1
stator-from-rotor
7.49877
52.4147
1
stator-out
7.49900
48.1866
2
rotor-in
6.52730
41.2246
2
rotor-to-stator
6.52654
49.6560
2
stator-from-rotor
6.52655
49.3205
2
stator-out
6.52679
42.1989
3
rotor-in
5.73755
36.2369
3
rotor-to-stator
5.73652
47.8475
3
stator-from-rotor
5.73655
47.4376
3
stator-out
5.73631
37.9116
4
rotor-in
5.00422
31.6054
4
rotor-to-stator
5.00291
46.5088
4
stator-from-rotor
5.00291
46.0763
4
stator-out
5.00243
34.6346
5
rotor-in
4.51377
28.5078
5
rotor-to-stator
4.51200
45.5939
5
stator-from-rotor
4.51200
44.9160
5
stator-out
4.51158
32.6462
velocityMagnitudeProfile 1 1

Circumferential and Meridional Angle

Point Nr.
Interface Name
Flow Rate [ m3/s ]
Circumferential Angle [ deg ]
Meridional Angle [ deg ]
1
rotor-in
7.49939
144.584*
0*
1
rotor-to-stator
7.49875
132.331*
0.0464189*
1
stator-from-rotor
7.49877
65.2205
-0.0485770
1
stator-out
7.49900
82.3060
0.0666473
2
rotor-in
6.52730
148.212*
0*
2
rotor-to-stator
6.52654
133.359*
0.161646*
2
stator-from-rotor
6.52655
57.3408
0.0263715
2
stator-out
6.52679
79.5700
-1.29472
3
rotor-in
5.73755
151.392*
0*
3
rotor-to-stator
5.73652
134.440*
0.557902*
3
stator-from-rotor
5.73655
50.6392
0.301485
3
stator-out
5.73631
75.8818
-4.17130
4
rotor-in
5.00422
154.533*
0*
4
rotor-to-stator
5.00291
135.470*
1.43093*
4
stator-from-rotor
5.00291
44.1305
1.08400
4
stator-out
5.00243
71.6978
-7.74421
5
rotor-in
4.51377
156.736*
0*
5
rotor-to-stator
4.51200
137.213*
1.91191*
5
stator-from-rotor
4.51200
40.1407
1.25165
5
stator-out
4.51158
68.5492
-9.45562

Blade to Blade View

 
Meshes:1
Hub patches:1:rotor-hub
Shroud patches:1:rotor-shroud
Field:URel,LIC
Span:0.5

bladeToBladeView 1 1 1 1 1
bladeToBladeView 1 2 1 1 1
bladeToBladeView 1 3 1 1 1
bladeToBladeView 1 4 1 1 1
bladeToBladeView 1 5 1 1 1

Meridional Average

 
Meshes:1
Field:pTot

 

1 3

2 3

3 3

4 3
5 3


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