Numerical Investigation on Flow Structure Characteristics of a Supersonic Split Line Nozzle

TONG Yue; ZHENG Qing; ZOU Jie; LI Xiuming; CHEN Zhenyang

doi:10.15892/j.cnki.djzdxb.2019.04.026

TONG Yue, ZHENG Qing, ZOU Jie, LI Xiuming, CHEN Zhenyang

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2019, Vol. 39 ›› Issue (4) : 109-113.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2019, Vol. 39 ›› Issue (4) : 109-113. DOI: 10.15892/j.cnki.djzdxb.2019.04.026

Numerical Investigation on Flow Structure Characteristics of a Supersonic Split Line Nozzle

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2019, 39(4): 109-113 https://doi.org/10.15892/j.cnki.djzdxb.2019.04.026

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Received	Published
2018-08-29	2019-08-20
Issue Date
2025-05-19

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