摘要粉末燃料冲压发动机作为一种新兴火箭发动机技术得到了各个国家相关领域的广泛关注。自从上世纪40年代就有人提出相关的概念,由于当时的技术限制以及相关学科并不完善粉末燃料冲压发动机并没有得到大规模发展。76956
粉末燃料冲压发动机是一种结构简单、安全高效、易于维护的新型火箭发动机。本文主要分为三个部分对粉末燃料冲压发动机进行讨论。第一部分主要对发动机中的燃料供给系统进行了设计说明,供给系统作为发动机的重要组成部分有着不可代替的作用。第二部分对于粉末燃料的选择及其组分以及最佳工作环境进行了热力学计算并根据计算结果进行比较讨论。第三部分运用Fluent软件对发动机内部进行了模拟,分析出本文设计的发动机不同空气质量流率下燃烧室内温度、压强、马赫数的变化并对比分析。
毕业论文关键词 燃料供给系统 金属粉末燃料热力学计算 Fluent仿真
毕业设计说明书外文摘要
Title Ramjet design and numerical simulation of the powder fuel
Abstract Powder fuel ramjet rocket engine as a new technology has been widespread concern in the various countries in related fields。Since the 1940s it was suggested that the relevant concepts, because of technical limitations and related disciplines are not perfect powder fuel ramjet has not been large-scale development。
Powder fuel ramjet is a simple, safe and efficient, easy to maintain new rocket engines。 This paper is pided into three parts powder fuel ramjet discussion。The first part of the engine fuel supply system design notes, as an important part of the supply system of the engine has an irreplaceable role。The second part of the ingredients for the selection and the best working environment and the powder fuel thermodynamic calculations were discussed and compared according to the results。The third part of the Fluent software engine inside the simulation, analysis of the designed engine under different air mass flow rate of the combustion chamber temperature, pressure, Mach number change and comparative analysis。
Keywords Fuel supply system Metal powder fuel thermodynamic calculation Fluent simulation
目 录
1。绪论 3
1。1粉末燃料冲压发动机发展综述: 3
1。1。1粉末燃料冲压发动机简介: 3
1。1。2粉末燃料冲压发动机研究背景: 3
1。2国内外相关领域研究进展与发展经历 4
1。2。1概念提出 4
1。2。2国内外研究现状 4
1。3。现有技术的存在的问题 5
2。 粉末燃料冲压发动机燃料供给系统 6
2。1燃料供给系统简介 6
2。2传统气力输送系统介绍 6
2。3粉末冲压发动机燃料供给系统需求 8
2。4粉末冲压发动机燃料供给系统设计 9
2。5小结 10
3。燃料的热力学计算及其分析 10
3。1 CEA软件介绍 10
3。2燃料热力学计算基本目的 10
3。3燃料物质的选择 10 Fluent粉末燃料冲压发动机设计与数值模拟:http://www.youerw.com/jixie/lunwen_88358.html