Effect of Kerosene Dual-Jet Spacing on the Mixing and Combustion Characteristics of a Scramjet Combustor-Reference-Cited by-同舟云学术

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Effect of Kerosene Dual-Jet Spacing on the Mixing and Combustion Characteristics of a Scramjet Combustor

Published:2024-07-24 Issue:31 Volume:9 Page:33482-33493
ISSN:2470-1343
Container-title:ACS Omega
language:en
Short-container-title:ACS Omega

Author:

Peng Shuang-Shuang¹²^ORCID,Zhou Wen-Xuan³,Qi Yin-Yin⁴,Shi Hong-Hui¹,Li Ren-Wang¹,Zhu Lin³

Affiliation:

1. School of Mechanical Engineering, Zhejiang Sci-Tech University, Zhejiang 310018, China

2. School of Physics and Electronic Engineering, Fuyang Normal University, Fuyang 236041, China

3. Lab of Mechanical Structure & Biomechanics, Anhui Agricultural University, Hefei 230036, China

4. Hefei Gotion High-tech Power Energy Co., Ltd, Hefei 230036, China

Funder

Fuyang Normal University

Anhui Province

Anhui Province Photovoltaic Industry Common Technology Research Center Open Subjects

Publisher

American Chemical Society (ACS)

Link

https://pubs.acs.org/doi/pdf/10.1021/acsomega.4c00622

Reference36 articles.

1. Experimental and computational study on combustion performance of a kerosene fueled dual-mode scramjet engine

2. Effect of fuel injection distance and cavity depth on the mixing and combustion characteristics of a scramjet combustor with a rear-wall-expansion cavity

3. Influence of flow control schemes of the three-strut injector on the mixing efficiency and total pressure loss for a scramjet combustor

4. Numerical investigation of scale effect of various injection diameters on interaction in cold kerosene-fueled supersonic flow

5. Hydrogen/air supersonic combustion for future hypersonic vehicles

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