Email this article 
Parametric CFD designing of combustion chamber elements
- Authors: 1 11, 1 12, 1 11
-
Affiliations:
- Joint-Stock Company Saturn, Rybinsk
- NPO Saturn, Rybinsk
- Issue: Vol 5, No 1 (2006)
- Pages: 125-132
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/259
- DOI: https://doi.org/10.18287/2541-7533-2006-0-1%20(9)-125-132
- ID: 259
Cite item
Full Text
Abstract
The paper present a numerical and parametrical analysis of gas-turbine engine lines elements. The first part deals with the impact of the front device swirlers location and way of swirling on fuel-air mixing effectiveness in the lines. The second part offers a numerical analysis of the temperature pattern in the wake of secondary air jets and of mixing quality in the mixing area of the combustion chamber.
About the authors
1 1
Joint-Stock Company Saturn, Rybinsk
Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation
1 1
NPO Saturn, Rybinsk
Email: sadohina@ssau.ru
Russian Federation
1 1
Joint-Stock Company Saturn, Rybinsk
Email: sadohina@ssau.ru
Russian Federation
References
- Гупта А. Лилли Д. и др. Закрученные потоки / Пер с англ. - М.: Мир, 1987.
- CFX-TASCflow, v.2.12. User Documentation.
- ВасильевА. Ю., МайороваА. И., Свириденков А. А., Третьяков В. В., Ягодкин В. И. Исследование распыла топлива и смесеобразования в головной части камеры сгорания двигателей типа «НК». - Вестник СГАУ, № 2 (2), 2002 г.
- M. Blomeyer, B. Krautkremer, O. Haag, D. K. Hennecke, Secondary air mixing in a typical combustor flowfield, ISABE 99-7189, a99-34190.
Supplementary files
