This paper is concerned with the simulation of the unsteady turbulent flow and the aerodynamic tonal noise due to pressure fluctuations on the casing wall. Three-dimensional numerical simulations of the complete unsteady flow on the whole impeller-volute configuration were carried out using computational fluid dynamics (CFD) techniques. Pressure fluctuations on the casing wall were obtained, and the blade passing frequency (BPF) component was extracted to be modeled as the dipole source term of the wave equation. In a companion paper, the pressure fluctuations served as the external excitation to the casing vibration. Multi-domain direct boundary element method (BEM) was used to simulate the noise radiation with two domains representing the interior and exterior fields of the volute respectively, in order to take account of the sound scattering effect by the volute casing. Results showed that the dipole on the volute tongue surface was the most dominant noise source of the fan. Slopingedge volute tongue was introduced to reduce BPF noise radiation through phase cancellation between the dipole sources over the volute tongue.Key words: centrifugal fan; casing; blade passing frequency; acoustic dipole source
INTRODUCTIONCentrifugal fans, pumps and compressors are widely employed for industrial and civilian use. Their noise has been studied extensively, and is customarily classified into aerodynamic noise and structural noise. The noise spectrum of a centrifugal fan is characterized by broadband noise with pronounced discrete frequency tones. The broadband component arises from random fluctuations in pressure over a wide range of frequencies, and is associated with turbulent flow in the inlet stream, in the boundary layer, and the wake behind the blade. The prevailing discrete frequency tones are caused by the interaction between the mean air flow leaving the impeller and the fan casing. Among them, the BPF component is usually the most noticeable. This paper focuses on the numerical study of the BPF casing aerodynamic noise of a centrifugal fan through CFD and computational aeroacoutics (CAA). The BPF component of the noise spectra about this centrifugal overwhelmingly dominated other frequencies. Its companion paper studies the BPF casing vibration-induced noise. CAA is concerned with the prediction of the aerodynamic sound source and the transmission of the generated sound. The approaches used to solve the aeroacoustic problems can be generally classified into two broad categories: direct computation and indirect, or hybrid, computation. The direct approach computes the sound together with its fluid dynamic source field by solving the compressible flow equations. In a hybrid approach, the computation of flow is decoupled from the computation of sound, which can be done in a post-processing step based on an aeroacoustic theory [24]. Although recent advances in CFD and in computer technology have made the