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27138

APPLICATION OF GENETIC ALGORITHMS WITH THE AID OF PANEL METHOD TO OPTIMIZE MISSILE AERODYNAMIC SHAPE

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Last updated: 24 Dec 2024

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Abstract

The use of genetic algorithms with the aid of the panel method to determine high-efficiency missile aerodynamic shape has been examined. The capability of these algorithms to determine highly efficient and robust missile aerodynamic designs is demonstrated by giving a variety of design variables and constraints. Results indicate that the genetic algorithm is clearly capable of designing aerodynamic shapes that perform well in either single or multiple goal applications.

DOI

10.21608/asat.2011.27138

Keywords

Genetic Algorithm, Panel method, Missile, Optimization, CFD, Aerodynamic shape

Authors

First Name

Mutawkil

Last Name

Suliman

MiddleName

A.

Affiliation

Eng., Lecturer, Dpt. Of Mech. Aeronautical & Aerospace, Karary Academe of Technology, Khartoum, Sudan.

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Volume

11

Article Issue

ASAT Conference, 17-19 May 2005

Related Issue

4906

Issue Date

2011-05-01

Receive Date

2019-02-14

Publish Date

2011-05-01

Page Start

31

Page End

42

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 11_Issue ASAT Conference, 17-19 May 2005_Pages 31-42.pdf

PDF . 1.9MB

Link

https://asat.journals.ekb.eg/article_27138.html

Detail API

https://asat.journals.ekb.eg/service?article_code=27138

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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

APPLICATION OF GENETIC ALGORITHMS WITH THE AID OF PANEL METHOD TO OPTIMIZE MISSILE AERODYNAMIC SHAPE

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Article

Created At

22 Jan 2023