journal article·2025-03-01Open access

Numerical investigation of the multi-physics coupling effect of supersonic projectile on the cross section of terminal ballistics

L. Shen, D. Chen, H. Sun, Z. Yang

AIP Advances· Volume 15· Issue 3

Abstract

This study numerically investigates the multi-physics coupling effects of supersonic projectiles on terminal ballistics, focusing on shock wave interactions and their impact on measurement accuracy. A novel acoustic-optic coupling detection method is introduced, capable of capturing refractive index changes induced by shock waves. Using COMSOL simulations, the research demonstrates that this method offers superior sensitivity compared to traditional approaches, providing a precise way to determine projectile incidence angles. The findings have significant implications for improving measurement accuracy in hypersonic weapon systems.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Computational Fluid Dynamics and Aerodynamics · Electromagnetic Launch and Propulsion Technology · Guidance and Control Systems

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

School of Defence Science and Technology, Xi’an Technological University , No. 2 Xuefu Middle Road, Weiyang District, Xi’an City, Shaanxi Province 710021,

Funding

Xi’an Technological University

References (22)

Show source-provided references
1. Modelling the unsteady lift of a pitching NACA 0018 aerofoil using state-space neural networks10.1017/jfm.2024.148 ↗
2. The dynamics of supersonic flow past a new cusped leading edge airfoil10.1504/pcfd.2024.135636 ↗
3. Numerical investigation of aero-optical effects around the turret based on delayed detached eddy simulation and unsteady Reynolds averaged Navier–Stokes10.1177/09544100231207568 ↗
4. Seeker head geometric parameters influence on the hypersonic aero-optical effect10.1364/ao.491713 ↗
5. Target parameter detection and performance analysis based on sky screen and acoustic target10.19652/j.cnki.femt.2002349. ↗
6. Analysis on the speed properties of the shock wave in light curtain10.1515/phys-2022-0007 ↗
7. Effects of herringbone riblets on shock-wave/turbulent boundary-layer interactions10.1016/j.ast.2024.108914 ↗
8. Performance of flat-plate aluminum structures subjected to in-contact underwater explosions10.1016/j.jfluidstructs.2024.104084 ↗
9. Bend-twist coupling effects on the cavitation behavior and hydroelastic response of composite hydrofoils10.1016/j.ijmultiphaseflow.2022.104286 ↗
10. Aerodynamic characteristics of supersonic rocket-sled involving waverider geometry10.3390/app12157861 ↗
11. Numerical study of unsteady compressible flow induced by multiple pods operating in the hyperloop system10.1016/j.jweia.2022.105024 ↗
12. Experimental investigation on aero-optics of supersonic turbulent boundary layers10.1364/ao.56.007604 ↗
13. The optical distortion mechanism in a nearly incompressible free shear layer10.1017/s0022112004009553 ↗
14. Computational study of optical distortions by separated shear layers and turbulent wakes10.1017/s0022112008005697 ↗
15. Numerical procedure to determine the performance and structural response of passive shock wave safety valves under blast loading10.1177/20414196231197702 ↗
16. Simulations of the optical diffraction patterns produced by the pressure field of a clinical shock wave source10.1088/1402-4896/ad6d13 ↗
17. Correction to the quantum relation of photons in the Doppler effect based on a special Lorentz violation model10.1016/j.rinp.2024.107920 ↗
18. Pressure feedback system for flow separation mitigation in scramjet intakes10.1016/j.compfluid.2024.106397 ↗
19. Damage behavior of the surrounding medium caused by different blast-induced dynamic and static loadings10.1016/j.engfracmech.2024.110409 ↗
20. Numerical study on the effect of air-assisted nozzle shape on kerosene spray and flow characteristics10.1016/j.ast.2024.109488 ↗
21. Numerical investigations of shock/boundary-layer interaction and control for Mach 2.5 flow in an axisymmetric inlet10.1016/j.ast.2024.109468 ↗
22. Validation of a two-fluid turbulence model in comsol multiphysics for the problem of flow around aerodynamic profiles10.1038/s41598-024-52673-5 ↗