Manufacture of a cooling path of an advanced design for the combustion chamber of a liquid rocket engine using additive technologies

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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Bibliographic Details
Main Authors: Сергій Вікторович Аджамський, Ганна Андріївна Кононенко, Ростислав Вячеславович Подольський
Format: Article
Language:English
Published: National Aerospace University «Kharkiv Aviation Institute» 2021-05-01
Series:Авіаційно-космічна техніка та технологія
Subjects:
адитивні технології
камера згоряння
внутрішні канали
кут нахилу
шорсткість
Online Access:http://nti.khai.edu/ojs/index.php/aktt/article/view/1414

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