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Performance comparison of full-scale ramjet and scramjet using boron-based propellant

This study investigates the performance boundaries of ramjet and scramjet engines fueled by boron-based propellant through full-scale engine modeling and three-dimensional computational fluid dynamics simulations. Results show that the performance boundary between ramjets and scramjets occurs near M...

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Hlavní autoři: Xianju Wu, Zhijun Wei, Yun Wang, Ling zhou, Yunhui Wang, Ningfei Wang
Médium: Artigo
Jazyk:Inglês
Vydáno: KeAi Communications Co., Ltd. 2026-02-01
Edice:Defence Technology
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On-line přístup:http://www.sciencedirect.com/science/article/pii/S2214914725002740
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