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
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