The Dualistic Linear Regression Model of HTPB Propellant's Elongation under Constant Strain

ZOU  Sisi; YAN  Cong; MA  Cenrui; XIA  Xunhui

doi:10.15892/j.cnki.djzdxb.2013.04.004

ZOU Sisi, YAN Cong, MA Cenrui, XIA Xunhui

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2013, Vol. 33 ›› Issue (4) : 131-133.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2013, Vol. 33 ›› Issue (4) : 131-133. DOI: 10.15892/j.cnki.djzdxb.2013.04.004

BALLISIIC AND AIRDYNAMICS

The Dualistic Linear Regression Model of HTPB Propellant's Elongation under Constant Strain

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2013, 33(4): 131-133 https://doi.org/10.15892/j.cnki.djzdxb.2013.04.004

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Received	Published
2012-12-06	2013-08-20
Issue Date
2025-05-26

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