Manufacture of a cooling path of an advanced design for the combustion chamber of a liquid rocket engine using additive technologies
The creation of complex structural elements of aircraft using additive technologies is promising and is widely used since such elements have many design and technological advantages over the collection of individual finished parts. However, it requires the solution of many scientific and technical p...
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| Auteurs principaux: | , , |
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| Format: | Artigo |
| Langue: | Inglês |
| Publié: |
National Aerospace University «Kharkiv Aviation Institute»
2021-05-01
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| Collection: | Авіаційно-космічна техніка та технологія |
| Sujets: | |
| Accès en ligne: | http://nti.khai.edu/ojs/index.php/aktt/article/view/1414 |
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