22nd AIAA/CEAS Aeroacoustics Conference 2016
DOI: 10.2514/6.2016-2948
|View full text |Cite
|
Sign up to set email alerts
|

Effects of Vane Sweep on Fan-Wake/Outlet-Guide-Vane Interaction Broadband Noise

Abstract: A method is developed for predicting broadband noise due to the fan-wake interacting with the downstream swept outlet-guide-vanes in turbofan jet engines. It is validated against the NASA Source Diagnostic Test data. Sweep effects on the source, on the response and on the unsteady lift coupling with the duct modes are discussed. The mechanisms of broadband noise reduction due to vane sweep are studied, and a simple model to account for sweep effects is proposed accordingly.

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

0
4
0

Year Published

2024
2024
2024
2024

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
(4 citation statements)
references
References 6 publications
0
4
0
Order By: Relevance
“…The blade is often split into segments (Strip Theory) and each segment is assumed to be a very thin flat plate with a local mean stagger angle and zero attacking angle (thin-flat-plate assumption). Based on above hypotheses, it is noted that the thin-flat-plate assumption of a fan blade is applicable, but the rationality of using it on a turbine blade is untraceable, let alone the prediction of turbine broadband noise using those broadband noise models [19,20].…”
Section: Two-flat-plates Assumptionmentioning
confidence: 99%
See 3 more Smart Citations
“…The blade is often split into segments (Strip Theory) and each segment is assumed to be a very thin flat plate with a local mean stagger angle and zero attacking angle (thin-flat-plate assumption). Based on above hypotheses, it is noted that the thin-flat-plate assumption of a fan blade is applicable, but the rationality of using it on a turbine blade is untraceable, let alone the prediction of turbine broadband noise using those broadband noise models [19,20].…”
Section: Two-flat-plates Assumptionmentioning
confidence: 99%
“…Then, substituting Equations ( 15)~ (17) and Equation (20) into Equation ( 12) can result in the final expression of the sound power spectrum function. This formula is suitable for the broadband noise prediction of a turbine with high blending angle.…”
Section: Turbine Broadband Noise Modelmentioning
confidence: 99%
See 2 more Smart Citations