![EveningTest 1 cfd support logo 1](https://www.cfdsupport.com/wp-content/uploads/2021/12/cfd-support-logo-1.png)
Hi, this is steady-state CFD simulation report of:
eveningTest
Created by TCFD® 18.10 on Sun Oct 21 22:35:28 2018
Simulation Stats
Number of Components [ – ] (
topology
) |
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Mesh Size [ cells ] (
details
) |
stator : 347424
rotor : 417780
Total : 765204 |
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( details ) |
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![EveningTest 3 plotFlowRate 1 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/plotFlowRate-1-1.png)
![EveningTest 4 residuum 1 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/residuum-1-1.png)
Efficiency
1:stator_inlet — 2:rotor_outlet
![EveningTest 5 flowRateVsEfficiency 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/flowRateVsEfficiency-1.png)
![EveningTest 6 efficiency 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/efficiency-1.png)
Torque
![EveningTest 7 flowRateVsTorque 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/flowRateVsTorque-1.png)
![EveningTest 8 torque 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/torque-1.png)
Axial Force
![EveningTest 9 flowRateVsAxialForce 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/flowRateVsAxialForce-1.png)
![EveningTest 10 axialForce 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/axialForce-1.png)
Total Pressure Difference
1:stator_inlet — 2:rotor_outlet
![EveningTest 11 flowRateVsTotalPressureDifference 1 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/flowRateVsTotalPressureDifference-1-1.png)
![EveningTest 12 totalPressureDifference 1 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/totalPressureDifference-1-1.png)
Total Pressure Ratio
1:stator_inlet — 2:rotor_outlet
![EveningTest 13 flowRateVsTotalPressureRatio 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/flowRateVsTotalPressureRatio-1.png)
![EveningTest 14 totalPressureRatio 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/totalPressureRatio-1.png)
Total Pressure per Interfaces
![EveningTest 23 totalPressureProfile 1 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/totalPressureProfile-1-1.png)
Total Temperature Difference
1:stator_inlet — 2:rotor_outlet
![EveningTest 24 flowRateVsTotalTemperatureDifference 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/flowRateVsTotalTemperatureDifference-1.png)
![EveningTest 25 totalTemperatureDifference 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/totalTemperatureDifference-1.png)
Total Temperature per Interfaces
![EveningTest 34 totalTemperatureProfile 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/totalTemperatureProfile-1.png)
Velocity Magnitude per Interfaces
![EveningTest 35 velocityMagnitudeProfile 1 1](https://www.cfdsupport.com/wp-content/uploads/2022/01/velocityMagnitudeProfile-1-1.png)
Circumferential and Meridional Angle
(*) Calculated from the relative velocity.
Blade to Blade View
Meshes: | 2 |
Hub patches: | 2:rotor_hub |
Shroud patches: | 2:rotor_shroud |
Field: | pTot |
Span: | 0.1 |
Meshes: | 2 |
Hub patches: | 2:rotor_hub |
Shroud patches: | 2:rotor_shroud |
Field: | pTot |
Span: | 0.5 |
Meshes: | 2 |
Hub patches: | 2:rotor_hub |
Shroud patches: | 2:rotor_shroud |
Field: | pTot |
Span: | 0.9 |
Meshes: | 2 |
Hub patches: | 2:rotor_hub |
Shroud patches: | 2:rotor_shroud |
Field: | URel,LIC |
Span: | 0.1 |
Meshes: | 2 |
Hub patches: | 2:rotor_hub |
Shroud patches: | 2:rotor_shroud |
Field: | URel,LIC |
Span: | 0.5 |
Meshes: | 2 |
Hub patches: | 2:rotor_hub |
Shroud patches: | 2:rotor_shroud |
Field: | URel,LIC |
Span: | 0.9 |
Design: HTML5 UP
TCFD® 18.10 license is issued for CFDSUPPORT Lubos Pirkl as Limited and will be valid until Oct 25, 2019.