contributor author | Yong Cho | |
contributor author | Ph.D. student | |
contributor author | Young J. Moon | |
date accessioned | 2017-05-09T00:10:34Z | |
date available | 2017-05-09T00:10:34Z | |
date copyright | May, 2003 | |
date issued | 2003 | |
identifier issn | 0098-2202 | |
identifier other | JFEGA4-27185#543_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/128601 | |
description abstract | The unsteady viscous flow fields of a cross-flow fan are computed by time-accurately solving the two-dimensional incompressible Navier-Stokes equations with the unstructured triangular mesh solver algorithms. Based on pressure fluctuation data acquired at the surfaces of 35 rotating blades and stabilizer, acoustic pressures are predicted by the Ffowcs Williams-Hawkings equation. The aerodynamic noise sources of the cross-flow fan are also identified by correlating the acoustic pressure fluctuations with the unsteady flow characteristics during one revolution of the impeller. The present method is applied to the uniform and random pitch fans to investigate their performance and aeroacoustic noise characteristics, especially the frequency modulation of the tonal noise at the blade passing frequency (BPF). | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Discrete Noise Prediction of Variable Pitch Cross-Flow Fans by Unsteady Navier-Stokes Computations | |
type | Journal Paper | |
journal volume | 125 | |
journal issue | 3 | |
journal title | Journal of Fluids Engineering | |
identifier doi | 10.1115/1.1568356 | |
journal fristpage | 543 | |
journal lastpage | 550 | |
identifier eissn | 1528-901X | |
keywords | Impellers | |
keywords | Noise (Sound) | |
keywords | Fans | |
keywords | Blades | |
keywords | Cross-flow | |
keywords | Computation | |
keywords | Sound pressure | |
keywords | Pressure | |
keywords | Rotating blades | |
keywords | Equations AND Fluctuations (Physics) | |
tree | Journal of Fluids Engineering:;2003:;volume( 125 ):;issue: 003 | |
contenttype | Fulltext | |