Numerical Simulation and Verification of Structural Integrity of Solid Propellant Charge under Temperature Cycling Load

HAN Wangshen; ZHOU Dongmo; XIE Xuyuan; ZHONG Shanwei; CHEN Hang

doi:10.15892/j.cnki.djzdxb.2025.05.009

HAN Wangshen, ZHOU Dongmo, XIE Xuyuan, ZHONG Shanwei, CHEN Hang

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2025, Vol. 45 ›› Issue (5) : 656-664.

PDF(3759 KB)

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2025, Vol. 45 ›› Issue (5) : 656-664. DOI: 10.15892/j.cnki.djzdxb.2025.05.009

Academic article

Numerical Simulation and Verification of Structural Integrity of Solid Propellant Charge under Temperature Cycling Load

{{article.zuoZhe_EN}}

Author information +

History +

HeighLight

Abstract

Key words

QR code of this article

Cite this article

EndNote

Ris (Procite)

Bibtex

Download Citations

{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2025, 45(5): 656-664 https://doi.org/10.15892/j.cnki.djzdxb.2025.05.009

References

List( Publishing order | Descend order by publishing year | Descend order by cited within ) Chart analysis

References

Funding

RIGHTS & PERMISSIONS

PDF(3759 KB)

Accesses

Citation

Detail

Sections

Recommended

Received	Published
2024-10-31	2025-10-20
Issue Date
2025-11-28

Please choose a citation manager

Content to export