Wind Tunnel Testing of a Detonation Ramjet Model at Approach Air Stream Mach Number 5.7 and a Stagnation Temperature of 1500 K

标题
Wind Tunnel Testing of a Detonation Ramjet Model at Approach Air Stream Mach Number 5.7 and a Stagnation Temperature of 1500 K
作者
关键词
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出版物
DOKLADY PHYSICAL CHEMISTRY
Volume 481, Issue 1, Pages 100-103
出版商
Pleiades Publishing Ltd
发表日期
2018-07-31
DOI
10.1134/s0012501618070035

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