Experimental and numerical investigation of aluminum particle combustion driven instability in solid rocket motors
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference54 articles.
1. A numerical investigation of the effects of hydrogen addition on combustion instability inside a partially-premixed swirl combustor;Nam;Appl. Therm. Eng.,2020
2. Pressure oscillations and instability of working processes in the combustion chambers of solid rocket motors;Emelyanov;Acta Astronaut.,2017
3. A review of active control approaches in stabilizing combustion systems in aerospace industry;Zhao;Prog. Aero. Sci.,2017
4. Active suppression of swirl-stabilized combustion instability;Liu;Fuel,2021
5. Thermodynamics-acoustics coupling studies on self-excited combustion oscillations maximum growth rate;Zhao;J. Therm. Sci.,2022
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