Investigation on the effect of the expansion angle in the strut-based supersonic combustor-Reference-Cited by-同舟云学术

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Investigation on the effect of the expansion angle in the strut-based supersonic combustor

Published:2023-02 Issue: Volume:133 Page:108095
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Li Xin^ORCID,Pan Yu,Liu Chaoyang^ORCID,Liu Xiao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference63 articles.

1. Supersonic combustion in air-breathing propulsion systems for hypersonic flight;Urzay;Annu. Rev. Fluid Mech.,2018

2. Characteristics of hydrogen jets in supersonic crossflow: large-eddy simulation study;Watanabe;J. Propuls. Power,2013

3. Comparative investigation of strut cavity and wall cavity in supersonic flows;Dhankarghare;Aerosp. Sci. Technol.,2022

4. Flowing residence characteristics in a dual-mode scramjet combustor equipped with strut flame holder;Qiu;Aerosp. Sci. Technol.,2020

5. Liquid-fueled strut-based scramjet combustor design: a computational fluid dynamics approach;Manna;J. Propuls. Power,2008

Cited by 5 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 on the effect of the leading angle of the strut on the stabilization characteristics of lifted jet flames;Acta Astronautica;2024-11

2. Investigation of hydrogen/air co-flow jet flame propagation mechanism in supersonic crossflow;Physics of Fluids;2024-07-01

3. Large eddy simulation of hydrogen/air co-flow jet flame in the strut-based supersonic combustor;Aerospace Science and Technology;2024-03

4. Study on the application of artificial neural network-based flamelet/progress variable model in supersonic combustion;AIP Advances;2023-11-01

5. Effects of lifted fuel injection using an upstream ramp of a cavity on scramjet combustion;Aerospace Science and Technology;2023-11

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