The impact of swirling flow strength on lean-dome LDI pilot mixers’ operability and emissions-Reference-Cited by-同舟云学术

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The impact of swirling flow strength on lean-dome LDI pilot mixers’ operability and emissions

Published:2019-12 Issue: Volume:109 Page:109840
ISSN:0894-1777
Container-title:Experimental Thermal and Fluid Science
language:en
Short-container-title:Experimental Thermal and Fluid Science

Author:

Ren Xiao,Xue Xin,Brady Kyle B.,Sung Chih-Jen,Mongia Hukam C.

Funder

National Research Council

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering

Reference38 articles.

1. Flying into the future: aviation emissions scenarios to 2050;Owen;Environ. Sci. Technol.,2010

2. ICAO environmental report, global emissions: Sustainable alternative fuels. Montreal, QC, Canada: International Civil Aviation Organization, 2016.

3. Emission characteristics of a model combustor for aero gas turbine application;Li;Exp. Therm Fluid Sci.,2016

4. Optical diagnostics of fuel–air mixing and vortex formation in a cavity combustor;Krishna;Exp. Therm Fluid Sci.,2015

5. Effects of multi-orifice configurations of the quench plate on mixing characteristics of the quench zone in an RQL-TVC model;Jiang;Exp. Therm Fluid Sci.,2017

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1. Effect of Injection Orifice Geometry on the combustion efficiency of a swirl stabilized Methane/Air combustor, at atmospheric pressure;AIAA SCITECH 2024 Forum;2024-01-04

2. Experimental Study on OH* Chemiluminescence and Emissions in the Single-Element Lean Direct Injection Combustor;Combustion Science and Technology;2023-12-28

3. Swirl rotation direction effects on lean direct injection pilot mixer performance: Experiments and LES modeling;Aerospace Science and Technology;2022-10

4. Influence of key geometrical features on the non-reacting flow of a Lean Direct Injection (LDI) combustor through Large-Eddy Simulation and a Design of Experiments;Aerospace Science and Technology;2022-07

5. Experimental and numerical investigation of non-reaction flow characteristics in a concentric staged dual-swirl combustor;Journal of Mechanical Science and Technology;2022-03-30

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