Expanding the scramjet operating envelope through oxygen enrichment
通过富氧扩大超燃冲压发动机的运行范围
基本信息
- 批准号:DP230102601
- 负责人:
- 金额:$ 41.23万
- 依托单位:
- 依托单位国家:澳大利亚
- 项目类别:Discovery Projects
- 财政年份:2023
- 资助国家:澳大利亚
- 起止时间:2023-10-10 至 2026-10-09
- 项目状态:未结题
- 来源:
- 关键词:
项目摘要
This project aims to investigate the benefits of expanding the operating envelope of scramjets to higher altitudes and speeds by enriching their fuel with oxygen. This is expected to enhance the performance and flexibility of hypersonic air-breathing engines designed to form the core of a more reliable and economical access to space system. Expected outcomes of this project are a validated understanding and mapping of how oxygen enrichment can augment scramjet thrust at high altitudes and speeds, and a performance evaluation of a launch system optimised for this approach. This could provide significant benefits to the performance of reusable, air-breathing launch technology, where Australia is leading the push towards commercialisation.
该项目旨在研究通过富氧燃料将超燃冲压发动机的运行范围扩大到更高的高度和速度的好处。预计这将提高高超音速吸气式发动机的性能和灵活性,该发动机旨在构成更可靠、更经济的进入太空系统的核心。该项目的预期成果是对富氧如何在高空和高速度下增强超燃冲压发动机推力的有效理解和绘图,以及针对该方法优化的发射系统的性能评估。这可以为可重复使用的吸气式发射技术的性能带来显着的好处,澳大利亚正在引领该技术的商业化。
项目成果
期刊论文数量(0)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
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Prof Vincent Wheatley其他文献
Prof Vincent Wheatley的其他文献
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{{ truncateString('Prof Vincent Wheatley', 18)}}的其他基金
The general Richtmyer-Meshkov instability in magnetohydrodynamics
磁流体动力学中的一般 Richtmyer-Meshkov 不稳定性
- 批准号:
DE120102942 - 财政年份:2012
- 资助金额:
$ 41.23万 - 项目类别:
Discovery Early Career Researcher Award
The converging shock driven Richtmyer-Meshkov instability in magnetohydrodynamics
磁流体动力学中汇聚激波驱动的 Richtmyer-Meshkov 不稳定性
- 批准号:
DP120102378 - 财政年份:2012
- 资助金额:
$ 41.23万 - 项目类别:
Discovery Projects
相似国自然基金
超燃冲压发动机进排气系统流场的PIV实验研究
- 批准号:50876042
- 批准年份:2008
- 资助金额:38.0 万元
- 项目类别:面上项目
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Experimental Performance Characterisation and Measurement of Unstart Force on a Scramjet Intake across the Operational Envelope
超燃冲压发动机整个运行范围内进气口的启动力的实验性能表征和测量
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Advanced Flow Prediction of Scramjet Intakes and Data-Driven Inverse Design
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进入太空的变马赫数超燃冲压发动机流路设计
- 批准号:
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- 资助金额:
$ 41.23万 - 项目类别:
Postgraduate Scholarships - Doctoral
Design of a Variable Mach Number Scramjet Flowpath for Access-to-Space
进入太空的变马赫数超燃冲压发动机流路设计
- 批准号:
502365-2017 - 财政年份:2018
- 资助金额:
$ 41.23万 - 项目类别:
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Design of a Variable Mach Number Scramjet Flowpath for Access-to-Space
进入太空的变马赫数超燃冲压发动机流路设计
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502365-2017 - 财政年份:2017
- 资助金额:
$ 41.23万 - 项目类别:
Postgraduate Scholarships - Doctoral
Hypervelocity Roughness-Induced Laminar-Turbulent Transition for Advanced Scramjet Flow Control
用于先进超燃冲压发动机流动控制的超高速粗糙度引起的层流-湍流转变
- 批准号:
DE140100932 - 财政年份:2014
- 资助金额:
$ 41.23万 - 项目类别:
Discovery Early Career Researcher Award
The science of scramjet propulsion
超燃冲压发动机推进科学
- 批准号:
DP130102617 - 财政年份:2013
- 资助金额:
$ 41.23万 - 项目类别:
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Design optimisation and physical behaviour of fuel injection and mixing for innovative scramjet concepts
创新超燃冲压发动机概念的燃料喷射和混合的设计优化和物理行为
- 批准号:
DE120102277 - 财政年份:2012
- 资助金额:
$ 41.23万 - 项目类别:
Discovery Early Career Researcher Award
Flow physics of porous wall fuel injection for scramjet combustion and drag reduction
用于超燃冲压发动机燃烧和减阻的多孔壁燃料喷射的流动物理
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