Temperature Boundary Layer in Nozzle Wall with High and Low Burning Temperature Combined Propellant

ZHANG  Ming; YANG  Xuyin; WU  Qiu

doi:10.15892/j.cnki.djzdxb.2016.02.022

ZHANG Ming, YANG Xuyin, WU Qiu

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2016, Vol. 36 ›› Issue (2) : 91-93.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2016, Vol. 36 ›› Issue (2) : 91-93. DOI: 10.15892/j.cnki.djzdxb.2016.02.022

ROCKETS TECHNOLOGY

Temperature Boundary Layer in Nozzle Wall with High and Low Burning Temperature Combined Propellant

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2016, 36(2): 91-93 https://doi.org/10.15892/j.cnki.djzdxb.2016.02.022

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