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25782

NORMAL PERFORATION OF THIN DURALUMIN PLATES AT ORDNANCE VELOCITIES

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Last updated: 04 Jan 2025

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Abstract

This paper describes an experimental investigation of ballistic perforation of thin duralumin plates struck by the standard 7.62 mm bullet. It also simulates experimentally obtained results using Ravid-Bodner two-dimensional analytical model (1983) for plates exhibiting plugging failure. Five impact velocities ran-ging from 220 to 700 m/s and plates of 1.6, 3 and 4 mm thickness are considered. The plates mechanical properties are also changed by a heat treatment procedure which consists of solution hardening followed by artificial ageing. It is found that the changes in projectile velocity drop and in its energy loss with impact velocity are qualitatively similar. It is also found that the penetration resistance of treated plates is generally greater than the as-received ones, although the former have smaller yield and ultimate strengths. The specific energy loss increases with the increase of plate thickness for the as-received duralumin plates, while it first decreases and :h,-en increases for the treated plates. Predicted responses employing the five-stage analytical model of Ravid and Bodner are also obtained and compared with experimentally obtained responses. Good agreement is generally obtained.

DOI

10.21608/asat.1991.25782

Authors

First Name

A.

Last Name

Riad

MiddleName

M.

Affiliation

Teaching Asst., Dept. of Weapons and Ammunition, M.T.C., Cairo, EGYPT.

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Orcid

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First Name

H.

Last Name

Yakout

MiddleName

-

Affiliation

Asst. Prof., Dept. of Weapons and Ammunition, M.T.C., Cairo, EGYPT.

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Orcid

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First Name

M.

Last Name

Abdel-Kader

MiddleName

S.

Affiliation

Asst. Prof., Dept. of Weapons and Ammunition, M.T.C., Cairo, EGYPT.

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City

-

Orcid

-

First Name

Y.

Last Name

Kresha

MiddleName

-

Affiliation

Associate Prof., Dept. of Weapons and Ammunition, M.T.C., Cairo, EGYPT.

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Orcid

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Volume

4

Article Issue

ASAT CONFLENCE 14-16 May 1991 , CAIRO

Related Issue

4667

Issue Date

1991-05-01

Receive Date

2019-01-23

Publish Date

1991-05-01

Page Start

315

Page End

326

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_25782.html

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https://asat.journals.ekb.eg/service?article_code=25782

Order

28

Type

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

NORMAL PERFORATION OF THIN DURALUMIN PLATES AT ORDNANCE VELOCITIES

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Article

Created At

22 Jan 2023