推进剂
羽流
航空航天工程
固体燃料火箭
火箭(武器)
辐射
燃烧
环境科学
机械工程
气象学
工程类
物理
光学
化学
有机化学
作者
Ullekh Pandey,Manoj Chacko,S. R. Shine
出处
期刊:Computational Thermal Sciences
日期:2018-01-01
卷期号:10 (3): 211-224
标识
DOI:10.1615/computthermalscien.2018024489
摘要
The present paper aims to bring all the research carried out in the field of modeling of plume radiation from solid rocket motors. The analytical and numerical procedure followed and major inferences drawn are reviewed in detail, and compared wherever possible. The review has been made through a discussion of the analysis methodologies and the factors that influence plume radiation from solid rocket motors. Historical perspective of prediction methodology of SRM plume radiation is brought out. Efforts are made to bring out the research carried out in combustion modeling of SRM propellant, Al2O3 particle size and thermo-optical property estimation, and methods of solutions for gas and particle radiation modeling. Critical gaps and recent progress made are highlighted for setting up the future direction of research.
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