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Zhurnal Tekhnicheskoi Fiziki, 2019 Volume 89, Issue 8, Pages 1213–1218 (Mi jtf5538)

This article is cited in 1 paper

Solids

Experimental and computational study of a high-speed collision of an aluminum striker with a solid and mesh obstacle

V. A. Kuzminab, S. I. Gerasimovabcd, A. V. Zubankovab, A. G. Sirotkinab, E. P. Akashevaa, R. V. Gerasimovab

a Federal State Unitary Enterprise "Russian Federal Nuclear Center — All-Russian Research Institute of Experimental Physics", Sarov, Nizhny Novgorod region
b Sarov Physics Institute
c Institute for Problems of Mechanical Engineering, Institute of Applied Physics, Russian Academy of Sciences, Nizhny Novgorod, Russia
d Nizhny Novgorod State Technical University

Abstract: The results of computational and experimental studies of peculiarities of the process of impact between the striker and obstacle, which imitates shield protection of spacecrafts, have been considered and pictures of fragmentation of the striker and obstacle have been obtained. The numerical calculations were carried out using the method of smooth particle hydrodynamics (SPH). In the experiments, the striker was accelerated using a two-stage light-gas gun; the state of the obstacle and striker at the moment of their interaction was controlled using an X-ray and high-speed video camera. The recording equipment was switched on using induction cross sections. The comparative analysis of the results of numerical simulations and experiments have been considered.

Keywords: simulated shield of the spacecraft, the high-speed collision, light-gas gun, method of induction sections.

Received: 08.02.2019
Revised: 08.02.2019
Accepted: 26.02.2019

DOI: 10.21883/JTF.2019.08.47893.44-19


 English version:
Technical Physics, 2019, 64:8, 1145–1150

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