Abstract
The paper presents a simple algorithm for design calculation of axial flow compressor of gas turbine. The algorithm enables calculation of characteristic dimensions and gas angels in compressor stages using real gas model. Preliminary and detailed calculation base on data from GTD-350 gas turbine, also calculated and measured dimension of bleeds are compared.
| Original language | English |
|---|---|
| Pages (from-to) | 207-216 |
| Number of pages | 10 |
| Journal | Mechanics and Mechanical Engineering |
| Volume | 15 |
| Issue number | 3 |
| Publication status | Published - 2011 |
Keywords
- Axial compressor
- Design
- Gas turbine
ASJC Scopus subject areas
- General Materials Science
- Automotive Engineering
- Mechanics of Materials
- Mechanical Engineering
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