Thrust Estimates of a Partially Filled Multi-Cycle Pulse Detonation Rocket Engine

array(2) { ["lab"]=> string(2) "72" ["publication"]=> string(3) "450" } Thrust Estimates of a Partially Filled Multi-Cycle Pulse Detonation Rocket Engine - 爆震推进实验室 | LabXing

爆震推进实验室

简介 Detonation-based Propulsion Laboratory

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2013

期刊 Int. J. Turbo Jet-Engines

作者 Ke Wang · Wei Fan

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卷 30
期 3
Walter de Gruyter GmbH
ISSN: 2191-0332
DOI: 10.1515/tjj-2013-0008

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