<< Click to Display Table of Contents >> Additional views |
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The following information can be displayed in the diffuser dialog using the "Additional views" button: |
3D model of the currently designed diffuser geometry as well as spiral surfaces.
Velocity ratio cOut / cIn |
Deceleration ratio |
Length L |
Length of the diffuser |
Angle to centerline φ |
Angle between connecting line impeller-center ↔ outlet branch center and diffuser start section |
Center distance C |
Distance from the h-line to the center point |
Cone angle ϑ |
Cone angle from DIn to DOut over the length L |
Max. theoretical cone angle ϑmax |
ϑmax=16.5°(DIn/2/L)½ , see Gülich, |
Radius of centerline R |
Radius of middle line (for radial diffuser only) |
Diffuser outlet center C |
Spatial position of diffuser outlet |
Equivalent diameter D |
Diameter of the equivalent circle at the diffuser inlet / outlet |
Area A |
Area at diffuser inlet / outlet |
Velocity c |
Velocity at the diffuser inlet / outlet |
Pressure p |
Pressure at the diffuser inlet / outlet |
Total pressure pt |
Total pressure at the diffuser inlet / outlet |
For turbines and compressor additional information is visible:
Temperature T |
Temperature at the diffuser inlet / outlet |
Total temperature Tt |
Total temperature at the diffuser inlet / outlet |
Density ρ |
Density at the diffuser inlet / outlet |
Mach Number Ma |
Mach Number at the diffuser inlet / outlet |
Spiral losses are predicted using the theory of Aungier [Outlet Volute only]:
Cone loss coefficient |
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Wall loss coefficient |
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Overall loss coefficient |
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Diffuser cross sections (z-r)
Area distribution (l-A)