Email this article 
Distribution calculation of dropwise – liquid and vaporous fuel in combustion chamber spray – type component
- Authors: Tretiyakov V.V.1
-
Affiliations:
- Центральный институт авиационного моторостроения им. П.И. Баранова, Москва
- Issue: Vol 5, No 2-2 (2006): Special Issue
- Pages: 136-141
- Section: TECHNICAL SCIENCES
- URL: https://journals.ssau.ru/vestnik/article/view/396
- DOI: https://doi.org/10.18287/2541-7533-2006-0-2-2(10)-136-141
- ID: 396
Cite item
Full Text
Abstract
This work devoted to investigation of frontal device with 3-stage swirler for low-emission combustion chamber. The numerical model includes the Reynolds equations and Lagrangian individual droplet equations. Fuel distribution calculations were made for any real engine regimes. The results show large difference in vapour and liquid fuel phase concenration distributions.
About the authors
V. V. Tretiyakov
Центральный институт авиационного моторостроения им. П.И. Баранова, Москва
Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation
References
Supplementary files
