Three-dimensional predictions of the rod wake-airfoil interaction noise by hybrid methods

Björn Greschner, Sven Peth, Young June Moon, Jung H. Seo, Marc C. Jacob, Frank Thiele

Research output: Chapter in Book/Report/Conference proceedingConference contribution

5 Citations (Scopus)

Abstract

Sound generated by an airfoil in the wake of a rod is predicted numerically by two different hybrid CFD/CAA approaches (Ma = 0.2). The configuration is a symmetric airfoil one chord downstream of a rod, whose wake contains both periodic and broadband vortical fluctuations. In particular, a significant broadening of the main Strouhal peak has been observed at subcritical vortex shedding conditions. This study addresses the overall ability of both CFD/CAA hybrid approaches to model broadband noise sources. The first approach computes the aerodynamic noise by solving the linearized perturbed compressible equations (LPCE) for the noise propagation, with the acoustic sources and hydrodynamic flow variables computed from the incompressible Large Eddy Simulation (iLES) using a computional grid of approximately 3 million grid cells and high-order compact finite difference schemes. The second approach uses the unsteady aerodynamic field of a compressible Detached Eddy Simulation (DES) and a Ffowcs Williams & Hawkings (FW-H) acoustic analogy formulation for the farfield noise calculations. The non-zonal DES approach solves either the unsteady Reynolds-averaged or spatially filtered Navier-Stokes equations by using a novel cubic explicit algebraic stress turbulence model based on a two-equation k-e model by Lien and Lechziner. An implicit formulation is used with second order accuracy and a grid of approximately 2.3 million cells. The results of these hybrid approaches are compared and subsequently validated with the measurements of Jacob et al. in the nearfield (HWA) and in the farfield (noise).

Original languageEnglish
Title of host publication14th International Congress on Sound and Vibration 2007, ICSV 2007
Pages1599-1610
Number of pages12
Volume2
Publication statusPublished - 2007 Dec 1
Event14th International Congress on Sound and Vibration 2007, ICSV 2007 - Cairns, QLD, Australia
Duration: 2007 Jul 92007 Jul 12

Other

Other14th International Congress on Sound and Vibration 2007, ICSV 2007
CountryAustralia
CityCairns, QLD
Period07/7/907/7/12

Fingerprint

airfoils
wakes
rods
grids
charge flow devices
acoustics
predictions
aerodynamic noise
vortices
unsteady aerodynamics
noise propagation
broadband
formulations
vortex shedding
turbulence models
interactions
large eddy simulation
cells
Navier-Stokes equation
simulation

ASJC Scopus subject areas

  • Acoustics and Ultrasonics

Cite this

Greschner, B., Peth, S., Moon, Y. J., Seo, J. H., Jacob, M. C., & Thiele, F. (2007). Three-dimensional predictions of the rod wake-airfoil interaction noise by hybrid methods. In 14th International Congress on Sound and Vibration 2007, ICSV 2007 (Vol. 2, pp. 1599-1610)

Three-dimensional predictions of the rod wake-airfoil interaction noise by hybrid methods. / Greschner, Björn; Peth, Sven; Moon, Young June; Seo, Jung H.; Jacob, Marc C.; Thiele, Frank.

14th International Congress on Sound and Vibration 2007, ICSV 2007. Vol. 2 2007. p. 1599-1610.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Greschner, B, Peth, S, Moon, YJ, Seo, JH, Jacob, MC & Thiele, F 2007, Three-dimensional predictions of the rod wake-airfoil interaction noise by hybrid methods. in 14th International Congress on Sound and Vibration 2007, ICSV 2007. vol. 2, pp. 1599-1610, 14th International Congress on Sound and Vibration 2007, ICSV 2007, Cairns, QLD, Australia, 07/7/9.
Greschner B, Peth S, Moon YJ, Seo JH, Jacob MC, Thiele F. Three-dimensional predictions of the rod wake-airfoil interaction noise by hybrid methods. In 14th International Congress on Sound and Vibration 2007, ICSV 2007. Vol. 2. 2007. p. 1599-1610
Greschner, Björn ; Peth, Sven ; Moon, Young June ; Seo, Jung H. ; Jacob, Marc C. ; Thiele, Frank. / Three-dimensional predictions of the rod wake-airfoil interaction noise by hybrid methods. 14th International Congress on Sound and Vibration 2007, ICSV 2007. Vol. 2 2007. pp. 1599-1610
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