Parametric study on mixing augmentation mechanism induced by cantilevered ramp injectors in a shock-induced combustion ramjet engine-Reference-Cited by-同舟云学术

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Parametric study on mixing augmentation mechanism induced by cantilevered ramp injectors in a shock-induced combustion ramjet engine

Published:2021-01 Issue: Volume:108 Page:106413
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Du Zhao-bo,Shen Chi-bing,Huang Wei,Yan Li,Liang Jian-han,Choubey Gautam

Funder

National Key R&D Program of China

National Natural Science Foundation of China

Natural Science Foundation of Hunan Province

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. Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustor;Wang;Int. J. Hydrog. Energy,2013

3. Flame characteristics in supersonic combustor with hydrogen injection upstream of cavity flameholder;Sun;J. Propuls. Power,2008

4. Scramjet engines: the first forty years;Curran;J. Propuls. Power,2001

5. Mixing-related frequency oscillation of combustion in an ethylene-fueled supersonic combustor;Wang;Proc. Combust. Inst.,2015

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