Aerodynamics of owl-like wing model at low reynolds numbers

Hikaru Aono; Katsutoshi Kondo; Taku Nonomura; Masayuki Anyoji; Akira Oyama; Kozo Fujii; Makoto Yamamoto

doi:10.2322/tjsass.63.28

Aerodynamics of owl-like wing model at low reynolds numbers

Hikaru Aono, Katsutoshi Kondo, Taku Nonomura, Masayuki Anyoji, Akira Oyama, Kozo Fujii, Makoto Yamamoto

Thermo Fluid Dynamics Division

Research output: Contribution to journal › Article › peer-review

6 Citations (Scopus)

Abstract

Aerodynamics of an owl-like wing model at low Reynolds numbers (Re = O(10^4-5)) are investigated using large-eddy simulations with high-resolution computational schemes. The airfoil shape of the owl-like wing model is constructed based on a cross-sectional geometry of the owl wing at 40% wingspan from the root. The chord-based Re ranges from 1.0

Original language	English
Pages (from-to)	8-17
Number of pages	10
Journal	Transactions of the Japan Society for Aeronautical and Space Sciences
Volume	63
Issue number	1
DOIs	https://doi.org/10.2322/tjsass.63.28
Publication status	Published - 2020

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Space and Planetary Science

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10.2322/tjsass.63.28

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title = "Aerodynamics of owl-like wing model at low reynolds numbers",

abstract = "Aerodynamics of an owl-like wing model at low Reynolds numbers (Re = O(104-5)) are investigated using large-eddy simulations with high-resolution computational schemes. The airfoil shape of the owl-like wing model is constructed based on a cross-sectional geometry of the owl wing at 40% wingspan from the root. The chord-based Re ranges from 1.0",

author = "Hikaru Aono and Katsutoshi Kondo and Taku Nonomura and Masayuki Anyoji and Akira Oyama and Kozo Fujii and Makoto Yamamoto",

note = "Funding Information: The authors wish to thank Dr. Tianshu Liu for fruitful discussion and comments. This research used computational resources of the supercomputer at Japan Aerospace Exploration Agency (JAXA) and the K supercomputer provided by AICS through the HPCI system research project (Project ID: hp170215).",

year = "2020",

doi = "10.2322/tjsass.63.28",

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T1 - Aerodynamics of owl-like wing model at low reynolds numbers

AU - Aono, Hikaru

AU - Kondo, Katsutoshi

AU - Nonomura, Taku

AU - Anyoji, Masayuki

AU - Oyama, Akira

AU - Fujii, Kozo

AU - Yamamoto, Makoto

N1 - Funding Information: The authors wish to thank Dr. Tianshu Liu for fruitful discussion and comments. This research used computational resources of the supercomputer at Japan Aerospace Exploration Agency (JAXA) and the K supercomputer provided by AICS through the HPCI system research project (Project ID: hp170215).

PY - 2020

Y1 - 2020

N2 - Aerodynamics of an owl-like wing model at low Reynolds numbers (Re = O(104-5)) are investigated using large-eddy simulations with high-resolution computational schemes. The airfoil shape of the owl-like wing model is constructed based on a cross-sectional geometry of the owl wing at 40% wingspan from the root. The chord-based Re ranges from 1.0

AB - Aerodynamics of an owl-like wing model at low Reynolds numbers (Re = O(104-5)) are investigated using large-eddy simulations with high-resolution computational schemes. The airfoil shape of the owl-like wing model is constructed based on a cross-sectional geometry of the owl wing at 40% wingspan from the root. The chord-based Re ranges from 1.0

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ER -

Aerodynamics of owl-like wing model at low reynolds numbers

Abstract

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