Effects of cracking reaction on supersonic film cooling using gaseous hydrocarbon fuel as coolant-Reference-Cited by-同舟云学术

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Effects of cracking reaction on supersonic film cooling using gaseous hydrocarbon fuel as coolant

Published:2020-05 Issue: Volume:171 Page:115134
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Zuo Jingying,Zhang Silong,Qin Jiang,Bao Wen,Cui Naigang,Liu Xiaoyong

Funder

National Natural Science Foundation of China

National Postdoctoral Program for Innovative Talents

China Postdoctoral Science Foundation

Shenzhen Technology Projects

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference40 articles.

1. Numerical investigations into heat transfer and film cooling effect on a transonic blade endwall;He;Appl. Therm. Eng.,2018

2. Experimental investigation of isoenergetic film-cooling flows with shock interaction;Marquardt;AIAA J.,2019

3. Effects of angled film-cooling on cooling performance in a GO2/GH2 subscale thrust chamber;Xiang;Appl. Therm. Eng.,2019

4. Influence of cooling-gas properties on film-cooling effectiveness in supersonic flow;Keller;J. Spacecr. Rock.,2015

5. C. Morris, J. Ruf, Validation of Supersonic Film Cooling Modeling for Liquid Rocket Nozzle Applications, in: 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. (2010) 6657. doi:10.2514/6.2010-6657.

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1. Large eddy simulation of boundary layer combustion of hydrogen and hydrocarbon fuel films in a modeled scramjet combustor;CHINESE J AERONAUT;2024

2. Numerical investigation of flow distribution and transpiration cooling performance in heterogeneous porous media with reacting coolant;Applied Thermal Engineering;2024-07

3. Large eddy simulation of boundary layer combustion of hydrogen and hydrocarbon fuel films in a modeled scramjet combustor;Chinese Journal of Aeronautics;2024-07

4. Numerical study of film cooling in single-element injector gaseous CH4/O2 rocket engine with coupled wall function;AIP Advances;2024-03-01

5. Study on heat transfer coupling mechanism of direct thermoelectric conversion with regenerative cooling for supersonic combustor applications;Applied Thermal Engineering;2024-02

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