Effect of recess length on flow dynamics in gas-centered liquid-swirl coaxial injectors under supercritical conditions-Reference-Cited by-同舟云学术

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Effect of recess length on flow dynamics in gas-centered liquid-swirl coaxial injectors under supercritical conditions

Published:2022-09 Issue: Volume:128 Page:107757
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Liwei^ORCID,Li Yixing^ORCID,Wang Xingjian,Yang Vigor

Funder

Air Force Office of Scientific Research

Georgia Institute of Technology

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference50 articles.

1. Atomization and Sprays, vol. 1040;Lefebvre,1988

2. Liquid Rocket Thrust Chambers: Aspects of Modeling, Analysis, and Design, vol. 200;Yang,2004

3. Combustion Instabilities in Gas Turbine Engines, vol. 210;Lieuwen,2005

4. Dynamics and stability of lean-premixed swirl-stabilized combustion;Huang;Prog. Energy Combust. Sci.,2009

5. Liquid-propellant rocket engine injector dynamics;Bazarov;J. Propuls. Power,1998

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3. Numerical investigation of supercritical combustion dynamics in a multi-element LOx–methane combustor using flamelet-generated manifold approach;Physics of Fluids;2023-11-01

4. Impact of spray dynamics on combustion instabilities investigated by changing the atomizer recess in a swirl combustor;Combustion and Flame;2023-06

5. Numerical investigation on the performance of internal flow and atomization in the recessed gas-centered swirl coaxial injectors;Aerospace Science and Technology;2022-10

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