Abstract

Repeated plate impact testing with impact stress well below the threshold spall-stress (2.6 GPa) on medium carbon steel was carried out to the identical target plate by impacting the flyer plate. Occurrence of spall damage under low-velocity repeated impact was evaluated nondestructively with a low frequency scanning acoustic microscope. We observed the spall damage distribution by the B- and C-scan images. In order to initiate the spall damage (voids in a ductile material or cracks in a brittle one) the particular value of threshold spall-stress should be exceeded what already belongs to a commonly accepted knowledge. Generally, the spall damage development is dependent on the amplitude and the duration of the stress pulse. If the stress is high and duration is long enough to create tensile failure of material, the voids or cracks nucleate along the spall plane, and consequently, they form macrocracks. Therefore, the spall damage does not create when the first impact stress is less than the threshold spall-stress. However, after the fifth low-velocity repeated impact test, the generation of the spall damage was detected, even if the impact stress (1.1–1.7 GPa) was lower than the threshold spall-stress (2.6 GPa).

Highlights

  • Spall damages, microvoids or microcracks, are nucleated by an intensive tensile stress pulse within a solid that has been impacted at high velocity

  • The aim of the present paper is to reveal with ultrasonic technique the nucleation of the spall damage under low-velocity repeated impacts on the identical target plate of medium carbon steel

  • It was found that the medium carbon steel requires 2.6 GPa to initiate the spall damage

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Summary

Introduction

Microvoids or microcracks, are nucleated by an intensive tensile stress pulse within a solid that has been impacted at high velocity. The extent of spall damage has been examined by destructive means, namely sectioning and polishing the sample and observation with an optical or scanning electron microscope [1,2,3]. These destructive methods are applied to neither actual structural parts nor investigation of the spall damage growth under repeated impacts on the identical sample. The present authors already demonstrated effectiveness of the non-destructive ultrasonic method for the evaluation of the spall damage and recovery in aluminum and medium carbon steel plates under repeated impacts [4]. The evolution/recovery of spall damage was examined by low frequency scanning microscopy and ultrasonic measurement

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