Experimental and Numerical Study on the Perforation Behavior of an Aluminum 6061-T6 Cylindrical Shell

Author:

Byun Seon-Woo1ORCID,Joo Young-Jung1,Lee Soo-Yong23,Kim Sang-Woo23ORCID

Affiliation:

1. Advanced Technology R&D Center, Design Analysis Team, Hanwha Aerospace, 6, Pangyo-ro 319beon-gil, Bundang-gu, Seongnam-si 13488, Gyeonggi-do, Republic of Korea

2. School of Aerospace and Mechanical Engineering, Korea Aerospace University, 76 Hanggongdaehak-ro, Goyang-si 10540, Gyeonggi-do, Republic of Korea

3. Research Institute for Aerospace Engineering and Technology, Korea Aerospace University, Goyang-si 10540, Gyeonggi-do, Republic of Korea

Abstract

The modified Johnson–Cook (MJC) material model is widely used in simulation under high-velocity impact. There was a need to estimate a strain rate parameter for the application to the impact analysis, where the method typically used is the Split Hopkinson bar. However, this method had a limit to the experiment of strain rate. This study proposed to estimate the strain rate parameter of the MJC model based on the impact energy and obtained a parameter. The proposed method of strain rate parameter calculation uses strain parameters to estimate from the drop weight impact and high-velocity impact experiments. Then, the ballistic experiment and analysis were carried out with the target of the plate and cylindrical shape. These analysis results were then compared with those obtained from the experiment. The penetration velocities of plates could be predicted with an error of a maximum of approximately 3.7%. The penetration shape of the cylindrical target has a similar result shape according to impact velocity and had an error of approximately 6%.

Funder

National Research Foundation of Korea

Ministry of Trade, Industry & Energy

Publisher

MDPI AG

Subject

General Materials Science

Reference27 articles.

1. Dynamic analysis of asymmetric bladed-rotors supported by anisotropic stator;Kim;J. Sound Vib.,2012

2. Effect of bypass ratio on optimal fan outer pressure ratio and performance for turbofan engines;Xue;Int. J. Aeronaut. Space Sci.,2019

3. Le, D. (1997). Evaluation of Light Weight Material Concepts for Aircraft Turbine Engine Rotor Failure Protection.

4. Containment tests and analysis of soft wall casing fabricated by wrapping Kevlar fabric around thin metal ring;He;Aerosp. Sci. Technol.,2017

5. Perforation of aero-engine fan casing by a single rotating blade;He;Aerosp. Sci. Technol.,2013

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