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INVESTIGATION OF THE EFFECT OF AIR HUMIDITY ON GAS TURBINE ENGINE PARAMETERS
The mathematical model of a turbo-shaft engine with a two-stage gas generator was obtained. This model is based on the multi-stage compressor blade – to - blade description, which makes it possible to evaluate the effect of air humidity on its performances. The characteristics of the axial multistag...
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| Hauptverfasser: | , |
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| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
National Aerospace University «Kharkiv Aviation Institute»
2017-11-01
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| Schriftenreihe: | Авіаційно-космічна техніка та технологія |
| Schlagworte: | |
| Online Zugang: | http://nti.khai.edu/ojs/index.php/aktt/article/view/514 |
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