Stability investigation of two-phase n-decane rotating detonation waves-Reference-Cited by-同舟云学术

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Stability investigation of two-phase n-decane rotating detonation waves

Published:2024-01 Issue: Volume:144 Page:108817
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhao Ningbo^ORCID,Shao Xiaofeng^ORCID,Zheng Hongtao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference66 articles.

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

2. Pulse detonation propulsion: challenges, current status, and future perspective;Roy;Prog. Energy Combust.,2004

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

4. Recent progress, development trends, and consideration of continuous detonation engines;Ma;AIAA J.,2020

5. To the question of energy use of detonation combustion;Zeldovich;J. Propul. Power,2006

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. Implementation and verification of an OpenFOAM solver for gas-droplet two-phase detonation combustion;Physics of Fluids;2024-08-01

2. Influence of inhomogeneous distribution of inflow equivalence ratio on oblique detonation morphology and characteristic;Physics of Fluids;2024-07-01

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