Research progress on solid-fueled Scramjet  

作　　者：Xiang ZHAO Zhixun XIA Likun MA Chaolong LI Chuanbo FANG Benveniste NATAN Alon GANY 

机构地区：[1]Department of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China [2]Qinghe Building Ding-3,Beijing 100085,China [3]Faculty of Aerospace Engineering,Technion-Israel Institute of Technology,Haifa 32000,Israel

出　　处：《Chinese Journal of Aeronautics》2022年第1期398-415,共18页中国航空学报（英文版）

基　　金：supported by the China Scholarship Council and the National Natural Science Foundation of China(Nos.2020JJ4665,51706241).

摘　　要：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.

关 键 词：Combustor performance Flame stabilization SELF-IGNITION Solid-fueled Scramjet Supersonic combustion ramjet 

分 类 号：V235.21[航空宇航科学与技术—航空宇航推进理论与工程]