Effect of geometry parameters on the hydrocarbon fuel flow rate distribution in pyrolysis zone of SCRamjet cooling channels-Reference-Cited by-同舟云学术

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Effect of geometry parameters on the hydrocarbon fuel flow rate distribution in pyrolysis zone of SCRamjet cooling channels

Published:2019-10 Issue: Volume:141 Page:1114-1130
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Jiang Yuguang,Qin Jiang,Chetehouna Khaled,Gascoin Nicolas,Bao Wen

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference76 articles.

1. SCRamjet engines: the first forty years;Curran;J. Propul. Power,2001

2. Literature survey for a first choice of a fuel-oxidiser couple for hybrid propulsion based on kinetic justifications;Gascoin;J. Anal. Appl. Pyrol.,2012

3. Thermodynamic analysis on optimum performance of SCRamjet engine at high Mach numbers;Zhang;Energy,2015

4. Experimental study on combustion modes and thrust performance of a staged-combustor of the SCRamjet with dual-strut;Yang;Acta Astronaut.,2016

5. Thermal behavior of an isolator with mode transition inducing back-pressure of a dual-mode SCRamjet;Yang;Chin. J. Aeronaut.,2017

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