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    Flow-Field Analysis of a Typical Hydrogen-Fueled Dual-Mode Scramjet Combustor

    Source: Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 003
    Author:
    Wei Huang
    ,
    Lin Ma
    ,
    Mohamed Pourkashanian
    ,
    Derek B. Ingham
    ,
    Shi-bin Luo
    ,
    Jun Liu
    ,
    Zhen-guo Wang
    DOI: 10.1061/(ASCE)AS.1943-5525.0000136
    Publisher: American Society of Civil Engineers
    Abstract: As one of the most promising propulsive systems for future hypersonic vehicles, the hydrogen-fueled dual-mode scramjet combustor has drawn the attention of an ever increasing number of researchers. The two-dimensional coupled implicit NS equations, the standard
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      Flow-Field Analysis of a Typical Hydrogen-Fueled Dual-Mode Scramjet Combustor

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    http://yetl.yabesh.ir/yetl1/handle/yetl/56281
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    contributor authorWei Huang
    contributor authorLin Ma
    contributor authorMohamed Pourkashanian
    contributor authorDerek B. Ingham
    contributor authorShi-bin Luo
    contributor authorJun Liu
    contributor authorZhen-guo Wang
    date accessioned2017-05-08T21:33:51Z
    date available2017-05-08T21:33:51Z
    date copyrightJuly 2012
    date issued2012
    identifier other%28asce%29as%2E1943-5525%2E0000136.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56281
    description abstractAs one of the most promising propulsive systems for future hypersonic vehicles, the hydrogen-fueled dual-mode scramjet combustor has drawn the attention of an ever increasing number of researchers. The two-dimensional coupled implicit NS equations, the standard
    publisherAmerican Society of Civil Engineers
    titleFlow-Field Analysis of a Typical Hydrogen-Fueled Dual-Mode Scramjet Combustor
    typeJournal Paper
    journal volume25
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000136
    treeJournal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 003
    contenttypeFulltext
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