Approaches to Combustion Simulation

Viatcheslav I. Naoumov, V. Krioukov, A. Abdullin, A. V. Demin
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引用次数: 0

Abstract

Combustion processes (that is, conversion of chemical energy of propellant components into thermal energy of combustion products) are typical for various engineering systems. Working volumes wherein these processes can occur may be represented by combustion chambers of liquid-propellant rocket engines (LPRE), solid-propellant rocket engines (SPRE), air-breathing engines (ABE) steam-gas generators, magnetohydrodynamic generators (MHD generators), boiler furnaces of thermal electric power stations, and cylinders of internal combustion engines (ICEs) [1]. Besides, further conversion of combustion products with chemical conversions can proceed also in aircraft and rocket engine nozzles, ICE exhaust systems, LPRE gas ducts, etc.
燃烧模拟方法
燃烧过程(即推进剂成分的化学能转化为燃烧产物的热能)是各种工程系统的典型过程。这些过程可能发生的工作体积可以由液体推进剂火箭发动机(LPRE)的燃烧室、固体推进剂火箭发动机(SPRE)、吸气式发动机(ABE)的蒸汽-气体发生器、磁流体动力发电机(MHD发电机)、热电站的锅炉炉和内燃机(ICEs)的气缸来表示。此外,燃烧产物的化学转化也可以在飞机和火箭发动机喷嘴、ICE排气系统、LPRE燃气管道等中进行进一步转化。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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