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Design optimisation and physical behaviour of fuel injection and mixing for innovative scramjet concepts

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
负责人:
Adj A/Prof Hideaki Ogawa
金额:
$26.91万
依托单位:
依托单位国家:
澳大利亚
项目类别:
Discovery Early Career Researcher Award
财政年份:
2012
资助国家:
澳大利亚
项目状态:
已结题
起止时间:
2012-03-19 至 2018-12-31

项目摘要

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中文摘要
翻译
超燃冲压发动机是卫星发射和高速飞行的潜在游戏规则改变者。制造或破坏它们的现象是复杂的,实现最佳设计具有巨大的挑战性。该项目结合了先进的优化技术和流动模拟,以发现和理解创新的超燃冲压发动机设计的最佳燃料喷射。
英文摘要
Scramjets are a potential game changer for satellite launch and high speed flight. The phenomena that will make or break them are complex, and achieving optimal designs is hugely challenging. This project combines advanced optimisation techniques and flow simulations to find, and understand, optimal fuel injection for innovative scramjet designs.
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