LAWS OF MULTIPHASE FLOW BEHAVIOR IN THE HELICOPTER GAS TURBINE ENGINE INLET DUCT
The results of finite element modeling of the airflow contains dust particles of various sizes in the helicopter gas turbine engine air inlet duck with mounted and dismounted dust protective device are given. The main laws of the behavior of multiphase flow in the gas turbine engine inlet duct in re...
Kaydedildi:
| Asıl Yazarlar: | , |
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| Materyal Türü: | Artigo |
| Dil: | Inglês |
| Baskı/Yayın Bilgisi: |
National Aerospace University «Kharkiv Aviation Institute»
2017-07-01
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| Seri Bilgileri: | Авіаційно-космічна техніка та технологія |
| Konular: | |
| Online Erişim: | http://nti.khai.edu/ojs/index.php/aktt/article/view/1293 |
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