Abstract
Smoothed Particle Hydrodynamics (SPH) method is widely used in hypervelocity impact analysis, but it is computationally inefficient for common multiplate structures, such as multi-shock, mesh double-bumper, and stuffed shields. To improve the efficiency and accuracy of the SPH method, a reconstruction framework is proposed, including a fragment identification method, a fragment mapping method, and a sequential modeling and simulation approach. In the reconstruction framework, the total impact simulation of a multiplate structure consisting of n plates is decomposed into n individual impacts on each plate. To reduce the computation for each impact, a fragment identification method and a fragment mapping method are developed. Fragments generated from the impact with the i-th plate (i < n) are identified and mapped to the near positions in front of the (i + 1)-th plate using a linear motion algorithm. To reduce the total computation time, a sequential modeling and simulation approach is introduced, only the fragments from the i-th impact and the SPH model of the (i + 1)-th plate of the multiplate structure are reconstructed and simulated sequentially, excluding the other plates. The results show a significant improvement in computational efficiency compared to the traditional SPH method. For a three-layer structure with a 100 mm spacing, the efficiency is 59.2 times larger, while for a double-layer structure with a 350 mm spacing, the efficiency is 201.74 times larger. Moreover, the interactions between fragments are considered in the reconstruction framework, thereby the accuracy of the simulation is also improved.
| Original language | English |
|---|---|
| Pages (from-to) | 8140-8157 |
| Number of pages | 18 |
| Journal | Advances in Space Research |
| Volume | 75 |
| Issue number | 11 |
| DOIs | |
| State | Published - 1 Jun 2025 |
Keywords
- Fragment Identification
- Fragment Mapping
- Hypervelocity Impact
- Multiplate Structure
- Reconstruction Framework
- Sequential Modeling and Simulation Approach
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