Forced ignition modeling of methane-ethylene mixtures in scramjet combustors-Reference-Cited by-同舟云学术

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Forced ignition modeling of methane-ethylene mixtures in scramjet combustors

Published:2024-05 Issue: Volume:263 Page:113383
ISSN:0010-2180
Container-title:Combustion and Flame
language:en
Short-container-title:Combustion and Flame

Author:

Ogawa Shinichiro^ORCID,Kobayashi Kan,Tomioka Sadatake

Publisher

Elsevier BV

Reference37 articles.

1. Flight experiment for the validation of new methodology to compensate the wind tunnel contamination problem;Tani,2019

2. Numerical study on combustion flow-path design for a scramjet flight experiment;Takahashi;Trans. JSASS Aerosp. Tech. Japan,2021

3. System analysis of a hydrocarbon-fueled RBCC engine applied to a TSTO launch vehicle;Tomioka;Trans. JSASS Aerosp. Tech. Japan,2014

4. Combustion and ignition of thermally cracked kerosene in supersonic model combustors;Fan;J. Prop. Power,2007

5. Development of hydrocarbon-fueled scramjet engines: the hypersonic technology (HyTech) program;Powell;J. Prop. Power,2001

Cited by 1 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. Effect of jet splitting using passive strut on the performance and thermoacoustic characteristics of a scramjet combustor;Physics of Fluids;2024-08-01

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