Method of presenting compressor characteristics in mathematical models of gas turbine enginer
- Authors: 1 11
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Affiliations:
- Ufa State Aviation Technical University
- Issue: Vol 5, No 3 (2006)
- Pages: 7-12
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/447
- DOI: https://doi.org/10.18287/2541-7533-2006-0-3(11)-7-12
- ID: 447
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