Coupled finite element-discrete element method (FEM/DEM) for modelling hypervelocity impacts-Reference-Cited by-同舟云学术

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Coupled finite element-discrete element method (FEM/DEM) for modelling hypervelocity impacts

Published:2023-02 Issue: Volume:203 Page:296-307
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Færgestad R.M.^ORCID,Holmen J.K.^ORCID,Berstad T.^ORCID,Cardone T.^ORCID,Ford K.A.,Børvik T.^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Meteorites and space travel;Whipple;Astron. J.,1947

2. Space station MMOD shielding;Christiansen;Acta Astronaut.,2009

3. Numerical simulation of hypervelocity impact problem for spacecraft shielding elements;Silnikov;Acta Astronaut.,2018

4. A reactive material double-bumper shield for centimeter sized projectile;Ren;Int. J. Impact Eng.,2021

5. Fragment identification and statistics method of hypervelocity impact SPH simulation;Xiaotian;Chin. J. Aeronaut.,2011

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1. A review of shielding systems for protecting off-earth structures from micrometeoroid and orbital debris impact;Acta Astronautica;2024-10

2. Fragment Identification Method Based on DBSCAN and Its Application in Hypervelocity Impact of Whipple Shield;International Journal of Aeronautical and Space Sciences;2024-09-01

3. Determining Peak Shock Pressure and Cratering due to Hypervelocity Meteoroid Impact on Lunar Structures for Engineering Design;Journal of Aerospace Engineering;2024-09

4. Pressure propagation mechanism of open-cell aluminium foam within a pipe under hypervelocity impact;Materials Today Communications;2024-08

5. A viscoelastic-viscoplastic thermo-mechanical model for polymers under hypervelocity impact;International Journal of Mechanical Sciences;2024-06

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