The Application of Reliability Optimization Method to Multidisciplinary Design Optimization of Cruise Missile

XIA  Qing; CAI  Hong; ZHANG  Shifeng

doi:10.15892/j.cnki.djzdxb.2010.01.015

XIA Qing, CAI Hong, ZHANG Shifeng

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (1) : 40-42.

PDF(327 KB)

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (1) : 40-42. DOI: 10.15892/j.cnki.djzdxb.2010.01.015

MISSILES AND GUIDANCE TECHNOLOGY

The Application of Reliability Optimization Method to Multidisciplinary Design Optimization of Cruise Missile

{{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}}, 2010, 30(1): 40-42 https://doi.org/10.15892/j.cnki.djzdxb.2010.01.015

References

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

References

Funding

RIGHTS & PERMISSIONS

PDF(327 KB)

Accesses

Citation

Detail

Sections

Recommended

Received	Published
2009-04-15	2010-02-20
Issue Date
2025-05-19

Please choose a citation manager

Content to export