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Investigations on the Influence of the In-Stream Pylon and Strut on the Performance of a Scramjet Combustor

Parent resource - MTP - Mixing Enhancement

DOI - 10.1155/2014/309387
Journal Name - The Scientific World Journal
Publisher Name - Hindawi Limited
Document Type - journal-article

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Paper Abstract- The influence of the in-stream pylon and strut on the performance of scramjet combustor was experimentally and numerically investigated. The experiments were conducted with a direct-connect supersonic model combustor equipped with multiple cavities. The entrance parameter of combustor corresponds to scramjet flight Mach number 4.0 with a total temperature of 947 K. The research results show that, compared with the scramjet combustor without pylon and strut, the wall pressure and the thrust of the scramjet increase due to the improvement of mixing and combustion effect due to the pylon and strut. The total pressure loss caused by the strut is considerable whereas pylon influence is slight.


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Siddhant Gupta  

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  • The Scramjet Engine
    Corin Segal
 
 

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    Corin Segal

 
 

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