An improved flamelet/progress variable modeling in a hydrogen-fueled scramjet-Reference-Cited by-同舟云学术

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An improved flamelet/progress variable modeling in a hydrogen-fueled scramjet

Published:2023-07 Issue: Volume: Page:
ISSN:0360-3199
Container-title:International Journal of Hydrogen Energy
language:en
Short-container-title:International Journal of Hydrogen Energy

Author:

Tang Tao,Yu Jiangfei,Wang Zhenguo,Yang Daoning,Sun Mingbo,Wang Hongbo,Zhao Guoyan,Yang Yixin

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Energy Engineering and Power Technology,Condensed Matter Physics,Fuel Technology,Renewable Energy, Sustainability and the Environment

Reference76 articles.

1. Research progress on strut-equipped supersonic combustors for scramjet application;Chang;Prog Aero Sci,2018

2. Study on the characteristics of interaction flowfields induced by supersonic jet on a revolution body;Luo;Theoretical & Applied Mechanics Letters,2017

3. Mixing performance of transverse hydrogen/air multi-jet through coaxial injector arrays in supersonic crossflow;Zhang;Int J Hydrogen Energy,2021

4. Effect of hybrid coaxial air and hydrogen jets on fuel mixing at supersonic crossflow;Zhang;Int J Hydrogen Energy,2021

5. On the application of dynamic zone flamelet model to large eddy simulation of supersonic hydrogen flame;Yao;Int J Hydrogen Energy,2020

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