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离心风机气动次声的试验优化控制研究
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作者 黄其柏 王雪川 师汉民 《噪声与振动控制》 CSCD 1997年第3期18-21,共4页
本文提出了控制离心风机气动次声的方法,通过试验研究了欢声抑制规律,并利用正交试验方法对某空调器离心风机次声进行了优化控制。
关键词 风机 离心式风机 气动次声 优化控制
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A unified theory for gas dynamics and aeroacoustics in viscous compressible flows.PartⅡ.Sources on solid boundary 被引量:2
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作者 Feng Mao Luoqin Liu +3 位作者 Linlin Kang Jiezhi Wu Pengjunyi Zhang Zhenhua Wan 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2022年第12期58-66,共9页
This work attempts to extend the fundamental theory for classic gas dynamics to viscous compressible flow,of which aeroacoustics will naturally be a special branch.As a continuation of Part I.Unbounded fluid(Mao et al... This work attempts to extend the fundamental theory for classic gas dynamics to viscous compressible flow,of which aeroacoustics will naturally be a special branch.As a continuation of Part I.Unbounded fluid(Mao et al.,2022),this paper studies the source of longitudinal field at solid boundary,caused by the on-wall kinematic and viscous dynamic coupling of longitudinal and transverse processes.We find that at this situation the easiest choice for the two independent thermodynamic variables is the dimensionless pressure P and temperature T.The two-level structure of boundary dynamics of longitudinal field is obtained by applying the continuity equation and its normal derivative to the surface.We show that the boundary dilatation flux represents faithfully the boundary production of vortex sound and entropy sound,and the mutual generation mechanism of the longitudinal and transverse fields on the boundary does not occur symmetrically"at the samc level,but appears along a zigzag route.At the first level,it is the pressure gradient that generates vorticity unidirectionally;while at the second level,it is the vorticity that generates dilatation unidirectionally. 展开更多
关键词 Gasdynamics-aeroacoustics viscous compressible flow Advective wave equations Thermodynamic variables DILATATION Process splittingand coupling
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