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90916

Calculating Aerodynamic & Stability Characteristics for a MALE UAV using USAF Digital DATCOM

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Last updated: 04 Jan 2025

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Abstract

Motivated by the design of a MALE UAV for a military mission. The aerodynamic characteristics for the basic geometry of a UAV (MALE configuration) are calculated using USAF Digital DATCOM. Also, we calculated the aerodynamic characteristics of the UAV with deflected control surface for the same configuration. Furthermore, we estimate the stability and control derivative based on the required mission specification and flight envelope for the suggested design.

DOI

10.21608/iugrc.2017.90916

Authors

First Name

Nour ELdein

Last Name

Ibrahim

MiddleName

Ahmed

Affiliation

Aircraft Mechanics Department, Military Technical College, Cairo, Egypt.

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City

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Orcid

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First Name

Mohamed

Last Name

Zakaria

MiddleName

Y.

Affiliation

Aircraft Mechanics Department, Military Technical College, Cairo, Egypt.

Email

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City

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Orcid

-

First Name

Ahmed

Last Name

Elsebaie

MiddleName

Mohamed

Affiliation

Aircraft Mechanics Department, 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

63

Page End

63

Link

https://iugrc.journals.ekb.eg/article_90916.html

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https://iugrc.journals.ekb.eg/service?article_code=90916

Order

58

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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

Calculating Aerodynamic & Stability Characteristics for a MALE UAV using USAF Digital DATCOM

Details

Type

Article

Created At

22 Jan 2023