Numerical study of hydrogen ratio effect on detonation initiation characteristics of aviation kerosene with hydrogen addition-Reference-Cited by-同舟云学术

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Numerical study of hydrogen ratio effect on detonation initiation characteristics of aviation kerosene with hydrogen addition

Published:2024-09 Issue: Volume:152 Page:109353
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Zhiwu^ORCID,Hui Yuxiang,Zhang Yang^ORCID,Xiao Jingtao,Qin Weifeng^ORCID,Yang Yuxuan

Publisher

Elsevier BV

Reference46 articles.

1. Effects of detonation initial conditions on performance of pulse detonation chamber-axial turbine combined system[J];Liu;Energy,2023

2. Effects of inert gas jet on the transition from deflagration to detonation in a stoichiometric methane-oxygen mixture[J];Cheng;Fuel,2021

3. Air-breathing pulsed detonation thrust module: numerical simulations and firing tests [J];Frolov;Aerosp. Sci. Technol.,2019

4. Prediction of detonation initiation in an air-breathing pulse detonation combustor utilizing a simplified ethylene-air reaction mechanism [J];Sun;Aerosp. Sci. Technol.,2022

5. Experimental investigation on pulse operation characteristics of rotating detonation rocket engine[J];Zhou;Fuel,2023

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