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22361

Theoretical and Computational Study of Pitching Airfoils at Different Operating Conditions

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Last updated: 04 Jan 2025

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Abstract

The aerodynamic features of pitching NACA0009 airfoil are explored in the present study. The objective is to investigate the impact of pitching mean angle of attack and amplitude on the temporal variation of airfoil aerodynamic coefficients. Numerical simulation results using a commercial CFD solver are compared with those of the analytical prediction approach. The results of both approaches are found in a good agreement. The evolution of the flowfield structure around the airfoil at the different operating conditions is presented.

DOI

10.21608/asat.2017.22361

Authors

First Name

M.

Last Name

Ossman

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Affiliation

Egyptian Armed Forces, Egypt.

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Orcid

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First Name

M.

Last Name

Ahmed

MiddleName

Y. M.

Affiliation

Egyptian Armed Forces, Egypt.

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Orcid

-

First Name

Amr

Last Name

Elnashar

MiddleName

-

Affiliation

Egyptian Armed Forces, Egypt.

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-

City

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Orcid

-

First Name

O.

Last Name

Abdel Hamid

MiddleName

E.

Affiliation

Egyptian Armed Forces, Egypt.

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Volume

17

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 17 – April 11 - 13, 2017

Related Issue

4266

Issue Date

2017-04-01

Receive Date

2018-12-19

Publish Date

2017-04-01

Page Start

1

Page End

14

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 17_Issue AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 17 &nd….pdf

PDF . 4.1MB

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https://asat.journals.ekb.eg/article_22361.html

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https://asat.journals.ekb.eg/service?article_code=22361

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Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

Theoretical and Computational Study of Pitching Airfoils at Different Operating Conditions

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Article

Created At

22 Jan 2023