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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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| 主要な著者: | , |
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| フォーマット: | Artigo |
| 言語: | Inglês |
| 出版事項: |
National Aerospace University «Kharkiv Aviation Institute»
2017-11-01
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| シリーズ: | Авіаційно-космічна техніка та технологія |
| 主題: | |
| オンライン･アクセス: | http://nti.khai.edu/ojs/index.php/aktt/article/view/514 |
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