Author:
INOUE OSAMU,HATAKEYAMA NOZOMU
Abstract
The sound generated by a circular cylinder in a flow at low Mach numbers is
investigated by direct solution of the two-dimensional unsteady compressible Navier–Stokes equations. Results show that sound pressure waves are generated primarily
by vortex shedding from the cylinder surface into its wake. When a vortex is shed
from one side of the cylinder, a negative pressure pulse is generated from that side
whereas a positive pressure pulse is generated from the other side; alternate vortex
shedding from the upper and lower sides of the cylinder produces negative and
positive pulses alternately and thus produces sound pressure waves on both sides.
The dipolar nature of the generated sound is confirmed; lift dipole dominates the
sound field. The Doppler effect is shown to play an important role at finite Mach
numbers. The direct solutions are also compared with the solutions obtained by
Curle's acoustic analogy. The results show that Curle's solution describes well not
only the generation mechanism of the sound but also the propagation process if we
take the Doppler effect into consideration.
Publisher
Cambridge University Press (CUP)
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Cited by
267 articles.
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