Numerical Simulation of Compressor Stall Recovery Control

In order to explore the influencing factors of the effectiveness and stability for stall recovery and its flow mechanism when the antisurge valve is opened quickly, the dynamic stall recovery processes are simulated and the recovery processes at different discharging speeds are emphatically compared...

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Autor principal:	GAO Yuan, WU Yadong, OUYANG Hua
Formato:	article
Lenguaje:	ZH
Publicado:	Editorial Office of Journal of Shanghai Jiao Tong University 2021
Materias:	stall antisurge valve control distributed speed-changeable moore-greitzer model numerical simulation flow mechanism analysis Engineering (General). Civil engineering (General) TA1-2040 Chemical engineering TP155-156 Naval architecture. Shipbuilding. Marine engineering VM1-989
Acceso en línea:	https://doaj.org/article/1b3d523be82d445285a134c12aef7342
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id	oai:doaj.org-article:1b3d523be82d445285a134c12aef7342
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spelling	oai:doaj.org-article:1b3d523be82d445285a134c12aef73422021-12-03T02:59:23ZNumerical Simulation of Compressor Stall Recovery Control1006-246710.16183/j.cnki.jsjtu.2020.261https://doaj.org/article/1b3d523be82d445285a134c12aef73422021-11-01T00:00:00Zhttp://xuebao.sjtu.edu.cn/article/2021/1006-2467/1006-2467-55-11-1343.shtmlhttps://doaj.org/toc/1006-2467In order to explore the influencing factors of the effectiveness and stability for stall recovery and its flow mechanism when the antisurge valve is opened quickly, the dynamic stall recovery processes are simulated and the recovery processes at different discharging speeds are emphatically compared. Two numerical simulation methods, i.e., the distributed speed-changeable MG (Moore-Greitzer) model and the RANS (Reynolds Averaged Navier-Stokes) equation are used. The performance curves predicated by the two models agree well. The results of RANS show that the flow field changes are essentially the same when the valve is opened at different speeds. The disturbance, affected by the high-speed air flow generated at the inlet, moves downstream and finally reaches the leading edge of the rotor, whose scale will be further reduced with the impact of axial high-speed flow until completely dissipated. A comparison of different valve opening speeds indicates that the faster the valve is opened, the stronger the high-speed air flow generated at the inlet, shortening the stall recovery time. The greater the disturbance weakening degree, the faster the circumferential propagation speed of the disturbance, and the closer to the rotor speed. In the process of valve opening, the air flow fluctuation is more intense, and more energy is lost.GAO Yuan, WU Yadong, OUYANG HuaEditorial Office of Journal of Shanghai Jiao Tong Universityarticlestallantisurge valve controldistributed speed-changeable moore-greitzer modelnumerical simulationflow mechanism analysisEngineering (General). Civil engineering (General)TA1-2040Chemical engineeringTP155-156Naval architecture. Shipbuilding. Marine engineeringVM1-989ZHShanghai Jiaotong Daxue xuebao, Vol 55, Iss 11, Pp 1343-1351 (2021)
institution	DOAJ
collection	DOAJ
language	ZH
topic	stall antisurge valve control distributed speed-changeable moore-greitzer model numerical simulation flow mechanism analysis Engineering (General). Civil engineering (General) TA1-2040 Chemical engineering TP155-156 Naval architecture. Shipbuilding. Marine engineering VM1-989
spellingShingle	stall antisurge valve control distributed speed-changeable moore-greitzer model numerical simulation flow mechanism analysis Engineering (General). Civil engineering (General) TA1-2040 Chemical engineering TP155-156 Naval architecture. Shipbuilding. Marine engineering VM1-989 GAO Yuan, WU Yadong, OUYANG Hua Numerical Simulation of Compressor Stall Recovery Control
description	In order to explore the influencing factors of the effectiveness and stability for stall recovery and its flow mechanism when the antisurge valve is opened quickly, the dynamic stall recovery processes are simulated and the recovery processes at different discharging speeds are emphatically compared. Two numerical simulation methods, i.e., the distributed speed-changeable MG (Moore-Greitzer) model and the RANS (Reynolds Averaged Navier-Stokes) equation are used. The performance curves predicated by the two models agree well. The results of RANS show that the flow field changes are essentially the same when the valve is opened at different speeds. The disturbance, affected by the high-speed air flow generated at the inlet, moves downstream and finally reaches the leading edge of the rotor, whose scale will be further reduced with the impact of axial high-speed flow until completely dissipated. A comparison of different valve opening speeds indicates that the faster the valve is opened, the stronger the high-speed air flow generated at the inlet, shortening the stall recovery time. The greater the disturbance weakening degree, the faster the circumferential propagation speed of the disturbance, and the closer to the rotor speed. In the process of valve opening, the air flow fluctuation is more intense, and more energy is lost.
format	article
author	GAO Yuan, WU Yadong, OUYANG Hua
author_facet	GAO Yuan, WU Yadong, OUYANG Hua
author_sort	GAO Yuan, WU Yadong, OUYANG Hua
title	Numerical Simulation of Compressor Stall Recovery Control
title_short	Numerical Simulation of Compressor Stall Recovery Control
title_full	Numerical Simulation of Compressor Stall Recovery Control
title_fullStr	Numerical Simulation of Compressor Stall Recovery Control
title_full_unstemmed	Numerical Simulation of Compressor Stall Recovery Control
title_sort	numerical simulation of compressor stall recovery control
publisher	Editorial Office of Journal of Shanghai Jiao Tong University
publishDate	2021
url	https://doaj.org/article/1b3d523be82d445285a134c12aef7342
work_keys_str_mv	AT gaoyuanwuyadongouyanghua numericalsimulationofcompressorstallrecoverycontrol
_version_	1718373917229318144

Numerical Simulation of Compressor Stall Recovery Control

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