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23440

Simulating the Aerodynamic Heating of Gun-Launched Projectiles in Hypersonic Applications

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Last updated: 04 Jan 2025

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Abstract

A model was designed and built using The Mathworks' SIMULINK to simulate the aerodynamic heating of gun-launched projectiles ballistically flying at hypersonic velocities in the lower and upper atmosphere. The model is based on NASA Ames real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation. Developed model was used to predict the stagnation and surface temperatures of three conceptual projectiles intended for use as Navy Area Theater Ballistic Missile Defense (NATBMD) training targets.

DOI

10.21608/asat.2009.23440

Keywords

SIMULINK, exterior ballistics, Hypersonic Flight, aerodynamic heating, NATBMD

Authors

First Name

Hatem

Last Name

Daken

MiddleName

H.

Affiliation

Ph.D., Senior Structural Analysis Scientist/Engineer, Boeing Commercial Airplanes, The Boeing Company, Seattle, WA, USA (work was performed while working as the Principal Engineer, Defense Technology Inc., DTI, Arlington, VA, USA).

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Volume

13

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT- 13, May 26 – 28, 2009

Related Issue

4377

Issue Date

2009-05-01

Receive Date

2019-01-02

Publish Date

2009-05-01

Page Start

1

Page End

16

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 13_Issue AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT- 13, May….pdf

PDF . 292.0kB

Link

https://asat.journals.ekb.eg/article_23440.html

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https://asat.journals.ekb.eg/service?article_code=23440

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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

Simulating the Aerodynamic Heating of Gun-Launched Projectiles in Hypersonic Applications

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Article

Created At

22 Jan 2023