Effect of fan exit guide vane placement on fan broadband interaction noise

This paper explores the effect of fan exit guide vane (FEGV) placement on the aft-radiated interaction broadband noise created by the turbofan stage. The Source Diagnostic Test (SDT) rig-scale fan stage configurations are analyzed. Simulations are carried out using two low-order methods, one based on methods developed by Stewart Glegg and the other one based on methods developed by Ventres, allowing a comparison between their predictions. Additional effects, including the influence of vane sweep, inflow turbulence inhomogeneity and turbulence length scale estimation methods are investigated. The simulations presented here support previous findings that show, unlike the tonal noise, the broadband noise is only slightly affected by the FEGV placement. Both low-order models show that FEGV placement has a tilting effect on the broadband spectrum but they predict different trends in overall sound power level. The spectral tilting is mostly influenced by changes in the turbulence length scale while the overall change in the spectral level is associated with the changes in annulus area. Therefore, as the FEGV placement changes, the final spectrum depends on the magnitude of each influence. Still, the overall broadband noise level only varies within the range of 1 dB for all FEGV cases and placements considered.

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Publication Details

Journal
International Journal of Aeroacoustics
Published
2026-02-04
DOI
https://doi.org/10.1177/1475472x261419080
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
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article

Effect of fan exit guide vane placement on fan broadband interaction noise

Dmytro Voytovych, Craig A. Reimann, Julian Winkler, Nuo Li et al.
International Journal of Aeroacoustics
Aerodynamics and Acoustics in Jet Flows
article

Effect of fan exit guide vane placement on fan broadband interaction noise

Dmytro Voytovych, Craig A. Reimann, Julian Winkler, Nuo Li, Jeffrey M. Mendoza, Sheryl M. Grace
article en

Abstract

This paper explores the effect of fan exit guide vane (FEGV) placement on the aft-radiated interaction broadband noise created by the turbofan stage. The Source Diagnostic Test (SDT) rig-scale fan stage configurations are analyzed. Simulations are carried out using two low-order methods, one based on methods developed by Stewart Glegg and the other one based on methods developed by Ventres, allowing a comparison between their predictions. Additional effects, including the influence of vane sweep, inflow turbulence inhomogeneity and turbulence length scale estimation methods are investigated. The simulations presented here support previous findings that show, unlike the tonal noise, the broadband noise is only slightly affected by the FEGV placement. Both low-order models show that FEGV placement has a tilting effect on the broadband spectrum but they predict different trends in overall sound power level. The spectral tilting is mostly influenced by changes in the turbulence length scale while the overall change in the spectral level is associated with the changes in annulus area. Therefore, as the FEGV placement changes, the final spectrum depends on the magnitude of each influence. Still, the overall broadband noise level only varies within the range of 1 dB for all FEGV cases and placements considered.

International Journal of Aeroacoustics
Boston University (US), Isothermal Technology (United Kingdom) (GB)
Openalex Percentile: Top 66%
Aerodynamics and Acoustics in Jet Flows
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Effect of fan exit guide vane placement on fan broadband interaction noise — Dmytro Voytovych, Craig A. Reimann, et al. · International Journal of Aeroacoustics (2026) | TGRS Research Map | TGRS