![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 Mon Oct 22 19:29:50 2018
Simulation Stats
Number of Components [ – ] (
topology
) |
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Mesh Size [ cells ] (
details
) |
impeller : 456842
Total : 456842 |
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( details ) |
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![EveningTest 3 plotFlowRate 1 21](https://www.cfdsupport.com/wp-content/uploads/2021/12/plotFlowRate-1-21.png)
![EveningTest 4 residuum 1 20](https://www.cfdsupport.com/wp-content/uploads/2021/12/residuum-1-20.png)
Efficiency
1:Rotor_INFLOW — 1:Rotor_OUTFLOW
![EveningTest 5 flowRateVsEfficiency 1 19](https://www.cfdsupport.com/wp-content/uploads/2021/12/flowRateVsEfficiency-1-19.png)
![EveningTest 6 efficiency 1 19](https://www.cfdsupport.com/wp-content/uploads/2021/12/efficiency-1-19.png)
Torque
![EveningTest 7 flowRateVsTorque 1 12](https://www.cfdsupport.com/wp-content/uploads/2021/12/flowRateVsTorque-1-12.png)
![EveningTest 8 torque 1 12](https://www.cfdsupport.com/wp-content/uploads/2021/12/torque-1-12.png)
Axial Force
![EveningTest 9 flowRateVsAxialForce 1 12](https://www.cfdsupport.com/wp-content/uploads/2021/12/flowRateVsAxialForce-1-12.png)
![EveningTest 10 axialForce 1 12](https://www.cfdsupport.com/wp-content/uploads/2021/12/axialForce-1-12.png)
Total Pressure Difference
1:Rotor_INFLOW — 1:Rotor_OUTFLOW
![EveningTest 11 flowRateVsTotalPressureDifference 1 17](https://www.cfdsupport.com/wp-content/uploads/2021/12/flowRateVsTotalPressureDifference-1-17.png)
![EveningTest 12 totalPressureDifference 1 17](https://www.cfdsupport.com/wp-content/uploads/2021/12/totalPressureDifference-1-17.png)
Total Pressure Ratio
1:Rotor_INFLOW — 1:Rotor_OUTFLOW
![EveningTest 13 flowRateVsTotalPressureRatio 1 5](https://www.cfdsupport.com/wp-content/uploads/2021/12/flowRateVsTotalPressureRatio-1-5.png)
![EveningTest 14 totalPressureRatio 1 5](https://www.cfdsupport.com/wp-content/uploads/2021/12/totalPressureRatio-1-5.png)
Total Pressure per Interfaces
![EveningTest 19 totalPressureProfile 1 18](https://www.cfdsupport.com/wp-content/uploads/2021/12/totalPressureProfile-1-18.png)
Total Temperature Difference
1:Rotor_INFLOW — 1:Rotor_OUTFLOW
![EveningTest 20 flowRateVsTotalTemperatureDifference 1 4](https://www.cfdsupport.com/wp-content/uploads/2021/12/flowRateVsTotalTemperatureDifference-1-4.png)
![EveningTest 21 totalTemperatureDifference 1 4](https://www.cfdsupport.com/wp-content/uploads/2021/12/totalTemperatureDifference-1-4.png)
Total Temperature per Interfaces
![EveningTest 26 totalTemperatureProfile 1 4](https://www.cfdsupport.com/wp-content/uploads/2021/12/totalTemperatureProfile-1-4.png)
Velocity Magnitude per Interfaces
![EveningTest 27 velocityMagnitudeProfile 1 19](https://www.cfdsupport.com/wp-content/uploads/2021/12/velocityMagnitudeProfile-1-19.png)
Circumferential and Meridional Angle
(*) Calculated from the relative velocity.
Blade to Blade View
Meshes: | 1 |
Hub patches: | 1:Rotor_HUB |
Shroud patches: | 1:Rotor_SHROUD |
Field: | URel,LIC |
Span: | 0.1 |
Meshes: | 1 |
Hub patches: | 1:Rotor_HUB |
Shroud patches: | 1:Rotor_SHROUD |
Field: | URel,LIC |
Span: | 0.5 |