Effects of injection pressure variation on mixing in a cold supersonic combustor with kerosene fuel-Reference-Cited by-同舟云学术

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Effects of injection pressure variation on mixing in a cold supersonic combustor with kerosene fuel

Published:2017-10 Issue: Volume:139 Page:67-76
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Liu Wei-Lai,Zhu Lin,Qi Yin-Yin,Ge Jia-Ru,Luo Feng,Zou Hao-Ran,Wei Min,Jen Tien-Chien

Funder

National Natural Science Foundation of China

Anhui Provincial Natural Science Foundation

Key Project of Anhui Education Committee

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Nonlinear characteristics and detection of combustion modes for a hydrocarbon fueled scramjet;Zhang;Acta Astronaut.,2015

2. Effects of injection angle and pressure on mixing performance of fuel injection via various geometries for upstream-fuel-injected scramjets;Ogawa;Acta Astronaut.,2016

3. Turbulent burning of alcohol;Karpov;Combust. Explos. Shock.,1986

4. Parametric effects in a scramjet engine on the interaction between the air stream and the injection;Huang;Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng.,2012

5. Effect of the incident shock wave interacting with transversal jet flow on the mixing and combustion;Mai;Proc. Combust. Inst.,2011

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2. Evaluation of Influences of Changed Lower Cover Geometry on Kerosene–Air Interaction in a Scramjet Combustor;ACS Omega;2024-06-12

3. Investigations of the Atomization Characteristics and Mechanisms of Liquid Jets in Supersonic Crossflow;Aerospace;2023-11-27

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