
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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

Efficiency
1:stator_inlet — 2:rotor_outlet

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Torque

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Axial Force


Total Pressure Difference
1:stator_inlet — 2:rotor_outlet


Total Pressure Ratio
1:stator_inlet — 2:rotor_outlet


Total Pressure per Interfaces

Total Temperature Difference
1:stator_inlet — 2:rotor_outlet


Total Temperature per Interfaces
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Velocity Magnitude per Interfaces

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.