Effect of cavity back height on mixing efficiency of hydrogen multi-jets at supersonic combustion chamber-Reference-Cited by-同舟云学术

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Effect of cavity back height on mixing efficiency of hydrogen multi-jets at supersonic combustion chamber

Published:2020-10 Issue:51 Volume:45 Page:27828-27836
ISSN:0360-3199
Container-title:International Journal of Hydrogen Energy
language:en
Short-container-title:International Journal of Hydrogen Energy

Author:

Jiang Yu,Poozesh Amin,Marashi Seyed Maziar,Moradi R.,Barzegar Gerdroodbary M.^ORCID,Shafee Ahmad,Li Zhixiong,Babazadeh Houman

Funder

National Natural Science Foundation of China

Fundamental Research Funds for Central Universities of China

Australia ARC DECRA

Priority Academic Program Development of Jiangsu Higher Education Institutions

Science Fund of Key Laboratory of Hubei Province in Design and Test of Power System of Pure Electric Vehicle

Publisher

Elsevier BV

Subject

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

Reference62 articles.

1. Characteristics of dual transverse injection in scramjet combustor, part 1: mixing;Lee;J Propul Power,2006

2. The influence of upstream wavy surface on the mixing zone of the transverse hydrogen jet at supersonic free stream;Gerdroodbary;Aero Sci Technol,2019

3. The influence of the sinusoidal shock generator on the mixing rate of multi hydrogen jets at supersonic flow;Li;Aero Sci Technol,2020

4. Hydrogen fuel in scramjet engines-A brief review;Choubey;Int J Hydrogen Energy,2020

5. Molecular weight and injector configuration effects on the transverse injection flow field properties in supersonic flows;Huang;Aero Sci Technol,2014

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2. Effect of the arrangement of the injectors on the flow quantities in water injection into the hot supersonic crossflow inside the cylinder;International Journal of Modern Physics C;2024-05-07

3. Effect of upstream injection and pylon downstream of the cavity on the mixing characteristics;Physics of Fluids;2024-02-01

4. Influence of flow control schemes of the three-strut injector on the mixing efficiency and total pressure loss for a scramjet combustor;International Journal of Hydrogen Energy;2023-12

5. Effect of shock generator on fuel mixing in an annular single lobe transverse nozzle at the supersonic combustion chamber of a scramjet engine using computational fluid dynamics;Energy;2023-11

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