Experimental and numerical study of a full-size direct-connect dual-inlet DRE with a fuel-rich metalized solid propellant-Reference-Cited by-同舟云学术

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Experimental and numerical study of a full-size direct-connect dual-inlet DRE with a fuel-rich metalized solid propellant

Published:2019-09 Issue: Volume:140 Page:965-977
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:

Zhu Min,Chen Xiong,Zhou Chang-sheng,Xu Jin-sheng

Funder

National Natural Science Foundation of China

China Scholarship Council

Postgraduate Research & Practice Innovation Program of Jiangsu Province

NUST Outstanding Doctoral Funding

Publisher

Elsevier BV

Subject

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

Reference33 articles.

1. High mach number air-breathing engines (proceedings of the fourth agard colloquium on combustion and propulsion);Bragg;Int. J. Heat Mass Transf.,1963

2. Recent developments in ramjets, ducted rockets and scramjets;Timnat;Prog. Aerosp. Sci.,1990

3. A flow visualization facility for ducted rocket engine mixing studies;Brophy,1995

4. Swirl combustor flow visualization studies in a water tunnel;Schetz;J. Spacecraft Rockets,1983

5. Flow measurements in a model ramjet secondary combustion chamber;Chittilapilly;J. Propul. Power,1990

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