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90952

Preliminary Investigation on the Impact of Missile Design on its Aerodynamic Features

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Last updated: 24 Dec 2024

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Abstract

The dependence of aerodynamic features of a conventional missile on its configuration is examined. The features in concern are the zero-lift drag coefficient, the lift-curve slope and the center of pressure location. These coefficients are estimated using a home-made reliable tool that is used for conceptual design and preliminary sizing of rockets of simple shapes.

DOI

10.21608/iugrc.2017.90952

Authors

First Name

Mahmoud

Last Name

Abdel-Fattah

MiddleName

M.

Affiliation

Department of Aerospace Engineering, Military Technical College, Cairo, Egypt.

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Orcid

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First Name

Ahmed

Last Name

Hassan

MiddleName

E.

Affiliation

Department of Aerospace Engineering, Military Technical College, Cairo, Egypt.

Email

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City

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Orcid

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First Name

Mahmoud

Last Name

Ahmed

MiddleName

Y. M.

Affiliation

Department of Aerospace Engineering, Military Technical College, Cairo, Egypt.

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Volume

2

Article Issue

Second International Undergraduate Research Conference, IUGRC

Related Issue

13627

Issue Date

2017-07-01

Receive Date

2020-05-20

Publish Date

2017-07-01

Page Start

65

Page End

65

Article File

IUGRC_Volume 2_Issue Second International Undergraduate Research Conference, IUG….pdf

PDF . 504.3kB

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https://iugrc.journals.ekb.eg/article_90952.html

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https://iugrc.journals.ekb.eg/service?article_code=90952

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73

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Original Article

Type Code

762

Publication Type

Journal

Publication Title

The International Undergraduate Research Conference

Publication Link

https://iugrc.journals.ekb.eg/

MainTitle

Preliminary Investigation on the Impact of Missile Design on its Aerodynamic Features

Details

Type

Article

Created At

22 Jan 2023