Numerical study on the interaction between rotating detonation wave and turbine stator blades with multicomponent mixtures-Reference-Cited by-同舟云学术

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Numerical study on the interaction between rotating detonation wave and turbine stator blades with multicomponent mixtures

Published:2024-01 Issue: Volume:49 Page:1436-1445
ISSN:0360-3199
Container-title:International Journal of Hydrogen Energy
language:en
Short-container-title:International Journal of Hydrogen Energy

Author:

Shao Xiaofeng,Yang Honglei^ORCID,Zhao Ningbo,Zhai Dawei,Jin Shan,Zhang Wei,Zheng Hongtao

Publisher

Elsevier BV

Subject

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

Reference58 articles.

1. Rotating detonation combustors and their similarities to rocket instabilities;Anand;Prog Energ Combust,2019

2. Detonative propulsion;Wolański;Proc Combust Inst,2013

3. The formation and development of oblique detonation wave with different chemical reaction models;Guo;Aero Sci Technol,2021

4. Influence of incoming flow velocity and mixture equivalence ratio on oblique detonation characteristics;Guo;Aero Sci Technol,2021

5. Effect of inlet-valve structures on thrust of air-breathing pulse detonation engines;Chen;Propuls Power Res,2021

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Investigation of rotating detonation gas turbine cycle with different combustor passage areas;Aerospace Science and Technology;2024-10

2. The effect of CO content on CH4/CO/H2 rotating detonation wave propagation characteristics;Physics of Fluids;2024-08-01

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