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Subscripts

img72 2,img73 2,img74 2,img75 2    partial derivative with respect to axis directions and time
img76 1    at the wall
img77 1    asymptotic quantity
img78 1    turbulent
img79,img80,img81 1    reference directions
img82 1,img83 1,img84 1    related to x,y,z-axis direction
img85 2    reference value
img86 4    related to pressure
img87 1    related to momentum equations
img88    solvent part
img89    extra stress part

 

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Next: Input parameters Up: turbo-blade-post-user-manual Previous: ParaView License   Contents   Index

Turbo Unwrap filter

The filter Turbo Unwrap transforms the rotor region into a box according to a rather complicated set of rules. The purpose is to allow slicing the computational mesh and blades in the fixed relative distance between the hub and shroud patches. The filter can be applied to the whole computational mesh or to its individual parts (clips or e.g. only the blades). The unwrapping transformation is guided by hub and shroud patches.

TurboUnwrap properties

Figure: Turbo Blade Post; Filter properties.

Subsections

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Next: Preface Up: List of symbols Previous: Superscripts   Contents   Index

Subscripts

$ \color{white} a_x$, $ \color{white} a_y$, $ \color{white} a_z$, $ \color{white} a_t$    partial derivative with respect to axis directions and time
$ \color{white} a_w$    at the wall
$ \color{white} a_\infty$    asymptotic quantity
$ \color{white} a_T$    turbulent
$ \color{white} a_i$, $ \color{white} a_j$, $ \color{white} a_k$    reference directions
$ \color{white} a_1$, $ \color{white} a_2$, $ \color{white} a_3$    related to x,y,z-axis direction
$ \color{white} a_0$    reference value
$ \color{white} a_p$    related to pressure
$ \color{white} a_m$    related to momentum equations
$ \color{white} a_s$    solvent part
$ \color{white} a_e$    extra stress part

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Technical Specifications & Software Features

  • Both Linux & Windows OS compatible
  • Fully Automated
  • Compressible Flow
  • Turbulent Flow
  • Heat Transfer between Fluid and Solid Parts
  • Both Subsonic and Transonic
  • Fully Parallel Computing
  • Robust OpenFOAM® Solvers
  • Meshing using SnappyHexMesh
  • Smart external mesh import
  • Advanced Postprocessing
  • Convergence Monitoring
  • Special Boundary Conditions & Function Objects
Turbomachinery CFD radial turbine in graphical interface

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