报告人简介:
Professor Papamoschou obtained his Ph.D. from Roshko at Caltech in the late 80th
before joining UCI. His expertise is in turbulent mixing layers and jets and recently jet noise
measurement and reduction. He served as Chair of the Department of Mechanical and
Aerospace Engineering, Associate Dean and Iterim Dean of the School of Engineering of
UCI. More information about professor Papamoschou can be obtained from
http://supersonic.eng.uci.edu/cv_papamoschou.htm.
报告内容摘要:
This research is motivated by the need for physical models for the jet noise source
that can be incorporated in future predictive codes for aircraft noise. The emphasis is on
jets with high-subsonic velocities typical of modern turbofan engines. The basis for the
source model is fluid-mechanical, inspired by seminal results on the structure and instability
of shear layers. The resulting “wavepacket” source is an amplitude-modulated pressure
wave prescribed on a cylinder surrounding the jet, in the acoustic near field. To construct
the noise source model for a given frequency, the wavepacket is parameterized and the
parameters are determined by least-squares minimization of the difference between the
modeled and experimental sound intensity distributions in the acoustic far field. The
parameterization process can be applied simultaneously to all frequencies of interest
through the concept of the self-similar wavepacket, i.e., a wavepacket with universal shape
whose axial scale varies inversely with frequency. A stochastic extension of this concept
shows a connection between the shape of the far-field spectrum and the emission polar
angle. This relation indicates that the broadening of the spectrum with increasing polar
angle can be explained on the basis of a single noise source (the wavepacket), rather than
the prevailing model of two disparate noise sources, one coherent and the other incoherent.
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