Study on Numerical Simulation Methods for Hypervelocity Impact on Large-Scale Complex Spacecraft Structures
This paper aims to study the difference of results in breakup state judgment, debris cloud and fragment characteristic parameter during hypervelocity impact (HVI) on large-scale complex spacecraft structures by various numerical simulation methods. We compared the results of the test of aluminum pro...
| Glavni autori: | , , , , , |
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| Format: | Članak |
| Jezik: | English |
| Izdano: |
MDPI AG
2021-12-01
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| Serija: | Aerospace |
| Teme: | |
| Online pristup: | https://www.mdpi.com/2226-4310/9/1/12 |