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25389

THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SOME LATERAL CONTROL DERIVATIVES OF RECTANGULAR. WING

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Last updated: 04 Jan 2025

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Abstract

In the field of Appred Aerodynamics, the evaluation of aerodynamic derivatives is essential for analysis of stability and control of flying bodies. In the present work some of important stability and control derivatives are calculated theoretically for a rectangular wing in an incompressible flow The theoretical solution is realized on the basis of two different methods; the Multhopp's method and the Von& Lattice Method (VLM). An experimental evaluation of the calculated derivatives is also performed. The experimental study was carried out by the testing of a wing model in a general-purpose low speed wind tunnel. A good agreement was found between theoretical and experimental results.

DOI

10.21608/asat.1997.25389

Authors

First Name

M.

Last Name

El-Sharnoby

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Affiliation

Associate professor, Benha High Technology Institute, Benha, Egypt.

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First Name

Metwally

Last Name

Metwally

MiddleName

H.

Affiliation

Faculty member, Military Technical College, Cairo, Egypt.

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First Name

O

Last Name

Abdel-Hamid

MiddleName

E.

Affiliation

Prof. of Aerod) riar•ics, Military Technical College, Cairo, Egypt.

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Volume

7

Article Issue

ASAT Conf. 13-15 May 1997

Related Issue

4645

Issue Date

1997-05-01

Receive Date

2019-01-20

Publish Date

1997-05-01

Page Start

53

Page End

66

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_25389.html

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https://asat.journals.ekb.eg/service?article_code=25389

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5

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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 EXPERIMENTAL INVESTIGATION OF SOME LATERAL CONTROL DERIVATIVES OF RECTANGULAR. WING

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Article

Created At

22 Jan 2023