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Research progress on solid-fueled Scramjet 被引量:10
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作者 Xiang ZHAO Zhixun XIA +4 位作者 Likun MA Chaolong LI Chuanbo FANG Benveniste NATAN Alon GANY 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2022年第1期398-415,共18页
The solid-fueled Scramjet is an interesting option for supersonic combustion ramjet.It shows significant advantages such as simple fuel supply and compactness,avoiding the complex system of tanks and pipelines that en... The solid-fueled Scramjet is an interesting option for supersonic combustion ramjet.It shows significant advantages such as simple fuel supply and compactness,avoiding the complex system of tanks and pipelines that encountered in liquid-fueled Scramjets.The solid-fueled Scramjet could be the simplest air-breathing engine for the hypersonic flight regime.This paper presents a comprehensive and systematic review of the research progress on solid-fueled Scramjet in various institutes and universities.It summarizes a progress overview of three types of the solid-fueled Scramjet,which covers a wealth of landmark numerical and experimental results.Based on this,several relevant key technologies are proposed.Several inherent scientific issues are refined,such as the mixing mechanism of multi-phase flow and supersonic airflow,ignition and combustion mechanism of the condensed phase in a supersonic airflow,and coupling mechanism of gas and solid phase in a supersonic flow.Finally,the historical development trend is clarified,and some recommendations are provided for future solid-fueled Scramjet. 展开更多
关键词 Combustor performance Flame stabilization SELF-IGNITION Solid-fueled Scramjet Supersonic combustion ramjet
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火箭基组合循环发动机总体布局研究进展(英文) 被引量:4
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作者 Tian-tian ZHANG Zhen-guo WANG +2 位作者 Wei HUANG Jian CHEN Ming-bo SUN 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2019年第3期163-183,共21页
本综述从总体布局层面综述火箭基组合循环(RBCC)发动机在各个国家的发展现状,旨在展现该型发动机在单级入轨任务中的发展前景,为设计组合循环发动机以及进行空天往返任务规划提供参考。本文将RBCC按照构型特点进行归类并举例介绍,概述... 本综述从总体布局层面综述火箭基组合循环(RBCC)发动机在各个国家的发展现状,旨在展现该型发动机在单级入轨任务中的发展前景,为设计组合循环发动机以及进行空天往返任务规划提供参考。本文将RBCC按照构型特点进行归类并举例介绍,概述了发动机-机身一体化设计情况,并简要介绍了RBCC动力飞行器的任务规划和多目标优化方法。当前,尽管RBCC的研究面临着很多艰难的挑战,但是RBCC具有单级入轨的潜力,能够降低空天往返的成本。对RBCC发动机系统中各个子系统的研究也有利于促进其他相关学科的发展。 展开更多
关键词 火箭基组合循环发动机 单级入轨 空天往返 发动机-机身一体化
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