What system output files are available for assessing simulation results?

In addition to an updated restart file, Cloud Leo produces several turbomachinery-specific output files for your convenience:

Output File Type

Description

.CONVERGENCE Summary of solver settings used in a given simulation, as well as a convergence history of the residuals.
.OVERALL Contains history of performance data from the simulation as well as information regarding conservation
.MEANVALUE Summary of performance data for a given row at the last iteration conducted
.PSUF Contains a time history of pressure loading on the surface of the airfoil
.MIXEDAVG Summary of circumferentially averaged radial profiles at the inlet, exit, leading edge and trailing edge of a given airfoil row
.FORCES History of the forces acting on the airfoil as well as the power being added to or extracted from the system
.STATION Summary of flow data mass-averaged over I-planes up and downstream of the airfoil
.SURFDATA File for creating three-dimensional contour plots that are limited to the airfoil surface
.INOUT Summary of mass-averaged information about flow variables at the inlet and exit of the analysis domain
.LOAD Summary of flow properties on the airfoil surface at five different spanwise locations

 

For multi-row cases, two additional files are provided:

Output File Type

Description

-MPI-.OVERALL History of performance data for the entire multi-row simulation
-MPI-.MEANVALUE Summary of performance data for the last iteration of the entire multi-row simulation
Code
Author
George Fan
Date Created
2013-06-11 03:12:55
Date Updated
2013-06-23 06:48:35
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4033