High-fidelity numerical simulation of longitudinal thermoacoustic instability in a high-pressure subscale rocket combustor-Reference-Cited by-同舟云学术

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High-fidelity numerical simulation of longitudinal thermoacoustic instability in a high-pressure subscale rocket combustor

Published:2024-11 Issue: Volume:154 Page:109487
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Hasti Veeraraghava Raju^ORCID,Ranjan Reetesh

Publisher

Elsevier BV

Reference66 articles.

1. Dynamics and stability of lean-premixed swirl-stabilized combustion;Huang;Prog. Energy Combust. Sci.,2009

2. Comprehensive review of liquid-propellant combustion instabilities in f-1 engines;Oefelein;J. Propuls. Power,1993

3. Combustion instabilities coupled by pressure waves and their active control;Candel;Symp., Int., Combust.,1992

4. A review of active control of combustion instabilities;McManus;Prog. Energy Combust. Sci.,1993

5. Prediction and control of combustion instabilities in real engines;Poinsot;Proc. Combust. Inst.,2017

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