Turboshaft gas turbine engine thermodynamics calculation method based on blade machine blade to blade description.Part III. Turbine parameters calculation
Blade-to-blade modeling of turbomachinery, based on methods for developing the parameters and characteristics of modern gas turbine engines, enables the resolution of a wide range of theoretically and practically significant problems in engine design, development, and operation. It also improves the...
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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»
2025-05-01
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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/2874 |
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