FEATURES OF HEAT TRANSFER IN THE GAS TURBINE ENGINE BEARING CHAMBER
The issue of ensuring the thermal regime of the rotor support, which guarantees reliable operation of the power plant, is particularly important in designing oil systems of aviation gas turbine engines, as well as ground-based GTEs. The exact calculation of the heat flux from the engine to the GTE b...
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| Principais autores: | , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
National Aerospace University «Kharkiv Aviation Institute»
2018-12-01
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| coleção: | Авіаційно-космічна техніка та технологія |
| Assuntos: | |
| Acesso em linha: | http://nti.khai.edu/ojs/index.php/aktt/article/view/350 |
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