Investigation of kerosene supersonic combustion performance with hydrogen addition and fuel additive at low Mach inflow conditions-Reference-Cited by-同舟云学术

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Investigation of kerosene supersonic combustion performance with hydrogen addition and fuel additive at low Mach inflow conditions

Published:2021-02 Issue: Volume:285 Page:119139
ISSN:0016-2361
Container-title:Fuel
language:en
Short-container-title:Fuel

Author:

Luo Feiteng,Song Wenyan,Chen Wenjuan,Long Yaosong

Funder

Huazhong University of Science and Technology

Publisher

Elsevier BV

Subject

Organic Chemistry,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering

Reference39 articles.

1. Tests of the JAPHAR dual mode ramjet engine;Dessornes;Aerosp Sci Technol,2005

2. Supersonic Combustion in Air-Breathing Propulsion Systems for Hypersonic Flight;Urzay;Annu Rev Fluid Mech,2018

3. Upper bounds on the flight speed of hydrocarbon-fueled scramjet-powered vehicles;Waltrup;J Propul Power,2012

4. Survey on the mode transition technique in combined cycle propulsion systems;Huang;Aerosp Sci Technol,2014

5. Experimental Investigation of Hydrocarbon fuel ignition in scramjet combustor;Wenyan;Chin J Aeronaut,2004

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3. Experimental study on the ignition delay characteristics of pyrolysis gas from kerosene with hydrogen peroxide addition;Case Studies in Thermal Engineering;2024-08

4. Kinetic Models of Combustion of Kerosene;Journal of Engineering Physics and Thermophysics;2024-04-19

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