2023
DOI: 10.3390/aerospace10020191
|View full text |Cite
|
Sign up to set email alerts
|

The Submerged Nozzle Damping Characteristics in Solid Rocket Motor

Abstract: In this paper, the effects of the geometry of a submerged nozzle on the nozzle damping characteristics are studied numerically. Firstly, the numerical method is verified by the previous experimental data. Then, the mesh sensitivity analysis and the monitor position independence analysis are carried out. Thirdly, the effects of nozzle geometry on nozzle damping are systematically studied, and focuses are placed on the cavity size, convergent angle and divergent angle. The pulse decay method is utilized to evalu… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2

Citation Types

0
1
0

Year Published

2023
2023
2024
2024

Publication Types

Select...
4
1

Relationship

1
4

Authors

Journals

citations
Cited by 5 publications
(2 citation statements)
references
References 41 publications
0
1
0
Order By: Relevance
“…Energy conversion from heat to sound is desired in thermoacoustic engines [1][2][3], because there are no or fewer moving parts and non-exotic materials involved. When this occurs in most modern combustion equipment with high energy densities (such as in liquid/solid rocket engines [4][5][6], aero-engines [7][8][9], or land-based gas turbines [10][11][12]), intense thermoacoustic oscillations may occur, which pose a significant risk due to destructive damage [13][14][15]. This may include, structural vibration fatigue, overloaded heating to the combustor walls, and even explosion.…”
Section: Introductionmentioning
confidence: 99%
“…Energy conversion from heat to sound is desired in thermoacoustic engines [1][2][3], because there are no or fewer moving parts and non-exotic materials involved. When this occurs in most modern combustion equipment with high energy densities (such as in liquid/solid rocket engines [4][5][6], aero-engines [7][8][9], or land-based gas turbines [10][11][12]), intense thermoacoustic oscillations may occur, which pose a significant risk due to destructive damage [13][14][15]. This may include, structural vibration fatigue, overloaded heating to the combustor walls, and even explosion.…”
Section: Introductionmentioning
confidence: 99%
“…Energy conversion from heat to sound is desired in thermoacoustic engines [1,2], because there are no moving parts or fewer moving parts and non-exotic materials involved. When this occurs in most modern combustion equipment with high energy densities (such as in liquid/solid rocket engines [3,4], aero-engines [5][6][7], or land-based gas turbines [8][9][10]), intense thermoacoustic oscillations may occur, which pose a significant risk due to destructive damage [11][12][13]. This may include structural vibration fatigue, overloaded heating to the combustor walls, and even explosion.…”
Section: Introductionmentioning
confidence: 99%