Experimental and numerical investigation of transverse combustion instability in a rectangle multi-injector rocket combustor-Reference-Cited by-同舟云学术

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Experimental and numerical investigation of transverse combustion instability in a rectangle multi-injector rocket combustor

Published:2023-12 Issue: Volume:213 Page:215-230
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Ren Yongjie,Guo Kangkang^ORCID,Feng Songjiang,Tong Yiheng,Lin Wei,Nie Wansheng

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference59 articles.

1. Liquid Rocket Engine Combustion Instability;Yang,1995

2. Experimental Investigation of High Frequency Combustion Instability in Cryogenic Oxygen-Hydrogen Rocket Engines;Hardi,2012

3. Combustion properties of gaseous CH4/O2 coaxial jet flames in a single-element combustor;Kim;Fuel,2016

4. The explanation of certain acoustical phenomena1;Rayleigh;Nat.,1878

5. Combustion instability of gaseous fuels in a continuously variable resonance chamber (CVRC);Yu,2008

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