2024
DOI: 10.1016/j.oceaneng.2024.117376
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Flow pattern- and forces-susceptibility to small attack angles for a rectangular cylinder

Lei Zhou,
Qingchi Zhu,
K.T. Tse
et al.
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Cited by 16 publications
(2 citation statements)
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“…With the increasing performance requirements of combustion chambers and increasingly stringent emission regulations [1][2][3][4], gas turbine combustion chambers are required to operate at high temperature and high pressure [5][6][7][8][9], which usually leads to the occurrence of combustion instability [10][11][12][13][14][15][16][17]. The combustion instability phenomenon will be accompanied by pressure pulsation and exothermic pulsation in the flow field inside the combustion chamber [18][19][20][21], which leads to vibration of the combustion chamber components and affects the safe operation of the engine [22][23][24].…”
Section: Introductionmentioning
confidence: 99%
“…With the increasing performance requirements of combustion chambers and increasingly stringent emission regulations [1][2][3][4], gas turbine combustion chambers are required to operate at high temperature and high pressure [5][6][7][8][9], which usually leads to the occurrence of combustion instability [10][11][12][13][14][15][16][17]. The combustion instability phenomenon will be accompanied by pressure pulsation and exothermic pulsation in the flow field inside the combustion chamber [18][19][20][21], which leads to vibration of the combustion chamber components and affects the safe operation of the engine [22][23][24].…”
Section: Introductionmentioning
confidence: 99%
“…Low oxygen content is detrimental to stable combustion [2][3][4][5], significantly reducing the combustion reaction rate and flame propagation speed in the afterburner [6][7][8]. Moreover, the incoming flow velocity in the afterburner is exceptionally high, and minor perturbations can potentially lead to combustion instability [9][10][11][12][13]. Combustion instability manifests as periodic pressure and temperature pulsations [14][15][16], posing a risk of severe mechanical vibration and localized overheating of the aero-engine.…”
Section: Introductionmentioning
confidence: 99%