Effect of Fuel Particle Size on the Stability of Swirl Stabilized Flame in a Gas Turbine Combustor-Reference-Cited by-同舟云学术

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Effect of Fuel Particle Size on the Stability of Swirl Stabilized Flame in a Gas Turbine Combustor

Published:2014-01-21 Issue:0 Volume:0 Page:
ISSN:2191-0332
Container-title:International Journal of Turbo & Jet-Engines
language:
Short-container-title:

Author:

Mishra R. K.,Kishore Kumar S.,Chandel Sunil

Abstract

AbstractCombustion stability is examined in a swirl stabilized aero gas turbine combustor using computational fluid dynamics. A 22.5° sector of an annular combustor is modeled for the study. Unstructured tetrahedral meshes comprising 1.2 × 10

Publisher

Walter de Gruyter GmbH

Subject

Aerospace Engineering

Link

https://www.degruyter.com/document/doi/10.1515/tjj-2014-0027/pdf

Cited by 17 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical simulations on the effect of swirler installation angle on outlet temperature distribution in gas turbine combustors;Applied Thermal Engineering;2024-03

2. Design and combustion characteristics analysis of a static shaft turbofan engine;International Journal of Turbo & Jet-Engines;2023-09-13

3. Combustor technology of high temperature rise for aero engine;Progress in Aerospace Sciences;2023-07

4. Simulation of Carbon Monoxide Emission during Combustion of a Liquid Fuel Injected by a Pressure Swirl Atomizer into the Combustion Chamber;Combustion, Explosion, and Shock Waves;2023-04

5. Computational Study of Combustion Process in a Gas Turbine Engine;Recent Advances in Thermofluids and Manufacturing Engineering;2022-10-01

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