Effects of injector recess on heat flux in a combustion chamber with cooling channels-Reference-Cited by-同舟云学术

Effects of injector recess on heat flux in a combustion chamber with cooling channels

Published:2014-08 Issue: Volume:37 Page:110-116
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Ahn Kyubok^ORCID,Kim Jong-Gyu,Choi Hwan-Seok

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Combustion dynamics of swirl coaxial injectors in fuel-rich combustion;Ahn;J. Propuls. Power,2012

2. Effects of injector recess and chamber pressure on combustion characteristics of liquid–liquid swirl coaxial injectors;Ahn;Combust. Sci. Technol.,2011

3. Fuel-rich combustion characteristics of biswirl coaxial injectors;Ahn;J. Propuls. Power,2011

4. Effects of recess length on discharge coefficients of swirl coaxial injectors;Ahn;Combust. Sci. Technol.,2012

5. Combustion instability and heat transfer in a subscale thrust chamber;Ahn,2013

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