Stats

  • State Not Answered
  • Replies 6
  • Subscribers 7
  • Views 3845
  • Members are here 0
More Content

Result of calculation in FineTurbo

DenysK

Dear colleagues,
I deal with 3D calculation of axial compressor in FineTurbo. I have done steady state calculation.
I have encoutered with such issue. On the stator blade, on the suction side I have zone with increased Total Pressure.
It doesn't corresponds to written in books about aerodynamics of compressor. I atteched one picture and added values of parameter in different places of section of stator blade.

Perhaps, can someone explain this result or I did something incorrectly?

  • 0 in reply to DenysK

    Apologies for the delayed reply. I have conducted a simulation of Tutorial Number 5, which involves a 1.5-stage axial compressor with 2 stators and one rotor. I have maintained all settings as specified in the post, including a total pressure range of 119500–132500 Pa and the blade-to-blade surface at mid-span. However, I have not encountered any anomalous outcomes.

Cadence Guidelines

Community Guidelines

The Cadence Design Communities support Cadence users and technologists interacting to exchange ideas, news, technical information, and best practices to solve problems and get the most from Cadence technology. The community is open to everyone, and to provide the most value, we require participants to follow our Community Guidelines that facilitate a quality exchange of ideas and information. By accessing, contributing, using or downloading any materials from the site, you agree to be bound by the full Community Guidelines.