Published August 1, 2018 | Version v1
Journal article

Ballistic impact analysis of double-layered metal plates

  • 1. Systems Engineering Department, Military Technological College, P.O Box 262 PC 111, Muscat, Sultanate of Oman (Oman)
  • 2. Aerospace Manufacturing Research Centre, Department of Aerospace Engineering, University Putra Malaysia, 43400 Serdang, Selangor (Malaysia)

Description

In the present study, ballistic impact analysis of double layered circular metal plates with different arrangements were investigated numerically using the finite element method. Nine different double layered plates configuration consist of steel 4340 (st), Aluminium 2014-T3 (Al), or titanium Ti-6A1-4V (Ti) having the same thickness were considered in this study and the energy absorption capability of each configuration were determined and compared. In order to validate the results obtained via the numerical method, an experimental ballistic test utilising a single stage gas gun was performed on single layer Al plates using a blunt projectile. It was found that the results obtained from numerical analysis agree well with the experimental results, which confirmed the accuracy of the numerical analysis procedure. The non-linear explicit finite element analysis employing Johnson-Cook plasticity material model coupled with was carried out using ABAQUS commercial package. A parametric study was conducted to determine the best configuration in terms of the energy absorption capability under ballistic impact. It was observed from the analysis that the double layered plate with titanium (front plate facing the projectile) and steel 4340 (back plate) produced the highest energy absorption with 279.72 J. However, the highest specific energy absorption (SEA) was given by titanium (front) and Aluminium (back) plate with 2830.45 J/kg. (paper)

Availability note (English)

Available from http://dx.doi.org/10.1088/1757-899X/405/1/012012

Additional details

Publishing Information

Journal Title
IOP Conference Series. Materials Science and Engineering (Online)
Journal Volume
405
Journal Issue
1
Journal Page Range
[8 p.]
ISSN
1757-899X

Conference

Title
7. AEROTECH Conference on Sustainability in Aerospace Engineering and Technology
Dates
7-8 Aug 2018
Place
Putrajaya (Malaysia)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
52094428
Subject category
S36: MATERIALS SCIENCE;
Resource subtype / Literary indicator
Conference
Descriptors DEI
ACCURACY; ALUMINIUM; ENERGY ABSORPTION; FINITE ELEMENT METHOD; NUMERICAL ANALYSIS; PARAMETRIC ANALYSIS; PLASTICITY; PLATES; STEELS; TITANIUM
Descriptors DEC
ABSORPTION; ALLOYS; CALCULATION METHODS; CARBON ADDITIONS; ELEMENTS; IRON ALLOYS; IRON BASE ALLOYS; MATHEMATICAL SOLUTIONS; MATHEMATICS; MECHANICAL PROPERTIES; METALS; NUMERICAL SOLUTION; SORPTION; TRANSITION ELEMENT ALLOYS; TRANSITION ELEMENTS