Increasing the efficiency and stability of fuel supply to the combustion chamber of a liquid rocket engine by spray nozzles
- 作者: Ageenko Y.I.1, Bubnova A.S.1
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隶属关系:
- Technological University named after twice Hero of the Soviet Union Pilot-Cosmonaut A.A. Leonov
- 期: 卷 23, 编号 2 (2024)
- 页面: 7-13
- 栏目: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journal-vniispk.ru/2542-0453/article/view/311457
- DOI: https://doi.org/10.18287/2541-7533-2024-23-2-7-13
- ID: 311457
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详细
In this paper, various configurations of jet nozzles are analyzed, as well as their design. The effects of the inlet chamfer of jet nozzles on their flow rate and range are considered. It is shown out that today it is expedient to make precision micro-holes of the nozzles using high-precision three-dimensional electric-erosion equipment. The optimal design parameters of jet nozzles are also determined.
作者简介
Yu. Ageenko
Technological University named after twice Hero of the Soviet Union Pilot-Cosmonaut A.A. Leonov
编辑信件的主要联系方式.
Email: yi.ageenko@mail.ru
Doctor of Science (Engineering), Professor of the Department of Engineering and Technology
俄罗斯联邦A. Bubnova
Technological University named after twice Hero of the Soviet Union Pilot-Cosmonaut A.A. Leonov
Email: annette.bubnova@mail.ru
ORCID iD: 0009-0008-1912-6400
Student of the Department of Engineering and Technology
俄罗斯联邦参考
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