Aeroacoustic Simulation of an Owl Wing Cross-section Using Computational Fluid Dynamics

In this study, we aim to investigate the low noise flights of owls in terms of aerodynamics. The flow around cross-section of an owl wing, which is known for its nearly silent flight, is numerically analyzed using Computational Fluid Dynamics (CFD). The analysis are based on the parameters of angle...

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Main Authors: Ferit Yıldız, Sedat Tokgoz
Format: Article
Language:English
Published: Sakarya University 2022-04-01
Series:Sakarya Üniversitesi Fen Bilimleri Enstitüsü Dergisi
Subjects:
Online Access:https://dergipark.org.tr/tr/download/article-file/1871794
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author Ferit Yıldız
Sedat Tokgoz
author_facet Ferit Yıldız
Sedat Tokgoz
author_sort Ferit Yıldız
collection DOAJ
description In this study, we aim to investigate the low noise flights of owls in terms of aerodynamics. The flow around cross-section of an owl wing, which is known for its nearly silent flight, is numerically analyzed using Computational Fluid Dynamics (CFD). The analysis are based on the parameters of angle of attack and the flight speed. The aerodynamic effects on the acoustic is compared in terms of vorticity and sound pressure level, where the frequency interval for the acoustic data is set to 0-7500Hz. It was seen that the vortical organisations around the airfoils are closely related to the acoustic results. The results show that the increase in both velocity and angle of attack affect the vorticity, thus lead to a rise in sound pressure level. It can be stated that the owl airfoil shape ensures a relatively silent flight.
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publisher Sakarya University
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series Sakarya Üniversitesi Fen Bilimleri Enstitüsü Dergisi
spelling doaj-art-da8badbfdc5c4143905687985f9bbdaf2025-08-20T02:31:52ZengSakarya UniversitySakarya Üniversitesi Fen Bilimleri Enstitüsü Dergisi2147-835X2022-04-0126237538710.16984/saufenbilder.96870128Aeroacoustic Simulation of an Owl Wing Cross-section Using Computational Fluid DynamicsFerit Yıldız0https://orcid.org/0000-0002-7450-846XSedat Tokgoz1https://orcid.org/0000-0002-0836-2861GEBZE TECHNICAL UNIVERSITYGEBZE TECHNICAL UNIVERSITYIn this study, we aim to investigate the low noise flights of owls in terms of aerodynamics. The flow around cross-section of an owl wing, which is known for its nearly silent flight, is numerically analyzed using Computational Fluid Dynamics (CFD). The analysis are based on the parameters of angle of attack and the flight speed. The aerodynamic effects on the acoustic is compared in terms of vorticity and sound pressure level, where the frequency interval for the acoustic data is set to 0-7500Hz. It was seen that the vortical organisations around the airfoils are closely related to the acoustic results. The results show that the increase in both velocity and angle of attack affect the vorticity, thus lead to a rise in sound pressure level. It can be stated that the owl airfoil shape ensures a relatively silent flight.https://dergipark.org.tr/tr/download/article-file/1871794aerodynamicsairfoilbiological flowcomputational fluid dynamics
spellingShingle Ferit Yıldız
Sedat Tokgoz
Aeroacoustic Simulation of an Owl Wing Cross-section Using Computational Fluid Dynamics
Sakarya Üniversitesi Fen Bilimleri Enstitüsü Dergisi
aerodynamics
airfoil
biological flow
computational fluid dynamics
title Aeroacoustic Simulation of an Owl Wing Cross-section Using Computational Fluid Dynamics
title_full Aeroacoustic Simulation of an Owl Wing Cross-section Using Computational Fluid Dynamics
title_fullStr Aeroacoustic Simulation of an Owl Wing Cross-section Using Computational Fluid Dynamics
title_full_unstemmed Aeroacoustic Simulation of an Owl Wing Cross-section Using Computational Fluid Dynamics
title_short Aeroacoustic Simulation of an Owl Wing Cross-section Using Computational Fluid Dynamics
title_sort aeroacoustic simulation of an owl wing cross section using computational fluid dynamics
topic aerodynamics
airfoil
biological flow
computational fluid dynamics
url https://dergipark.org.tr/tr/download/article-file/1871794
work_keys_str_mv AT ferityıldız aeroacousticsimulationofanowlwingcrosssectionusingcomputationalfluiddynamics
AT sedattokgoz aeroacousticsimulationofanowlwingcrosssectionusingcomputationalfluiddynamics