Calculating Annulus Area in a Compressor

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Discussion Overview

The discussion focuses on the concept of annulus area in compressors, specifically within the context of gas turbine engines. Participants explore its definition and relevance in performance analysis.

Discussion Character

  • Technical explanation, Conceptual clarification

Main Points Raised

  • One participant inquires about the definition of annulus area in a compressor.
  • Another participant suggests that it typically refers to the area between the cylinder and the piston, indicating a potential misunderstanding of the context.
  • A clarification is made regarding the specific context of annulus area in gas turbine engines, as opposed to reciprocating compressors.
  • A reference is provided to a technical document discussing compressor rotor performance and the annulus area as the space between the shaft and casing.
  • It is noted that the annulus area is defined as the flow area formed by two concentric circles, specifically the rotor and the compressor case.

Areas of Agreement / Disagreement

Participants express differing views on the definition of annulus area, with some focusing on its application in gas turbine engines while others reference more general definitions. The discussion remains unresolved regarding a singular definition applicable across different types of compressors.

Contextual Notes

There are limitations in the discussion regarding the assumptions made about the type of compressor being referenced and the definitions of terms used, which may vary across different contexts.

sid_galt
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What is annulus area in a compressor?
 
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It's not a general term as far as I know, but it can be the area between cylinder and the piston.
 
Sorry for being not clear. I was talking about the annulus area of a compressor in a gas turbine engine, not a reciprocating one.
 
It's the flow area in the compressor. It's an annulus because it is formed by two concentric circles i.e. the rotor and the compressor case.
 
Thanks for the help
 

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