Multi-point ignition of air/fuel mixture by the initiated subcritical streamer discharge-Reference-Cited by-同舟云学术

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Multi-point ignition of air/fuel mixture by the initiated subcritical streamer discharge

Published:2021-10 Issue: Volume: Page:
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Bulat Pavel,Chernyshov Pavel,Esakov Igor,Grachev Lev,Lavrov Pavel,Melnikova Anzhelika,Volkov Konstantin,Volobuev Igor

Funder

Ministry of Science and Higher Education of the Russian Federation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference45 articles.

1. Three-dimensional modeling of rotating detonation in a ramjet engine;Smirnov;Acta Astronaut.,2019

2. 3D numerical modeling of a cylindrical RDE with an inner body extending out of the nozzle;Betelin;Acta Astronaut.,2020

3. Numerical study of the reverse-rotating waves in rotating detonation engine with a hollow combustor;Liu;Acta Astronaut.,2020

4. A rotating detonation engine using methane-ethylene mixture and air;Wang;Acta Astronaut.,2021

5. Overview of performance, application,and analysis of rotating detonation engine technologies;Rankin;J. Propul. Power,2017

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. Interactions between microwaves and smart energetic materials: A review on emerging technologies for ignition and combustion enhancement;Chemical Engineering Journal;2024-10

2. Development of mathematical model and numerical simulation of plasma ignition of flammable mixture with microwave subcritical streamer discharge;Acta Astronautica;2023-03

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