Wind tunnel tests of a hydrogen-fueled detonation ramjet model at approach air stream Mach numbers from 4 to 8

出版年份 2017 全文链接

标题

作者

关键词

Detonation ramjet model, Wind tunnel, Supersonic airflow, Spinning detonation, Pulsed detonation, Fuel-based specific impulse

出版物

Volume 42, Issue 40, Pages 25401-25413

出版商

Elsevier BV

发表日期

2017-09-14

DOI

10.1016/j.ijhydene.2017.08.062

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