TY - JOUR
T1 - Research progress on solid-fueled Scramjet
AU - ZHAO, Xiang
AU - XIA, Zhixun
AU - MA, Likun
AU - LI, Chaolong
AU - FANG, Chuanbo
AU - NATAN, Benveniste
AU - GANY, Alon
N1 - Publisher Copyright:
© 2021
PY - 2022/1
Y1 - 2022/1
N2 - 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.
AB - 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.
KW - Combustor performance
KW - Flame stabilization
KW - Self-ignition
KW - Solid-fueled Scramjet
KW - Supersonic combustion ramjet
UR - http://www.scopus.com/inward/record.url?scp=85112814425&partnerID=8YFLogxK
U2 - 10.1016/j.cja.2021.06.002
DO - 10.1016/j.cja.2021.06.002
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AN - SCOPUS:85112814425
SN - 1000-9361
VL - 35
SP - 398
EP - 415
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 1
ER -