Performance evaluation of regenerative cooling/film cooling for hydrocarbon fueled scramjet engine-Reference-Cited by-同舟云学术

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Performance evaluation of regenerative cooling/film cooling for hydrocarbon fueled scramjet engine

Published:2018-07 Issue: Volume:148 Page:57-68
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

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

Funder

National Postdoctoral Program for Innovative Talents

China Postdoctoral Science Foundation

Heilongjiang Postdoctoral Fund

Innovative Research Groups

National Natural Science Foundation of China

Shenzhen Technology Projects

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference54 articles.

1. Effects of injection angle and pressure on mixing performance of fuel injection via various geometries for upstream-fuel-injected scramjets;Ogawa;Acta Astronaut.,2016

2. Numerical investigation of combustion field of hypervelocity scramjet engine;Zhang;Acta Astronaut.,2016

3. Investigation of flameholding characteristics in a kerosene-fueled scramjet combustor with tandem dual-cavity;hang Wang;Acta Astronaut.,2017

4. Drag and heat flux reduction mechanism of blunted cone with aerodisks;Huang;Acta Astronaut.,2017

5. Thermal behavior in the cracking reaction zone of scramjet cooling channels at different channel aspect ratios;Zhang;Acta Astronaut.,2016

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