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首页|期刊导航|热科学学报(英文版)|A new cascade-less engine operated from subsonic to hypersonic conditions: designed by computational fluid dynamics of compressible turbulence with chemical reactions

A new cascade-less engine operated from subsonic to hypersonic conditions: designed by computational fluid dynamics of compressible turbulence with chemical reactions

Ken Naitoh Kazushi Nakamura Takehiro Emoto

热科学学报(英文版)2010,Vol.19Issue(6):481-485,5.
热科学学报(英文版)2010,Vol.19Issue(6):481-485,5.DOI:10.1007/s11630-010-0412-y

A new cascade-less engine operated from subsonic to hypersonic conditions: designed by computational fluid dynamics of compressible turbulence with chemical reactions

A new cascade-less engine operated from subsonic to hypersonic conditions: designed by computational fluid dynamics of compressible turbulence with chemical reactions

Ken Naitoh 1Kazushi Nakamura 1Takehiro Emoto1

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摘要

关键词

Aircraft engine/multijets/twister system/compressible flow

Key words

Aircraft engine/multijets/twister system/compressible flow

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Ken Naitoh,Kazushi Nakamura ,Takehiro Emoto..A new cascade-less engine operated from subsonic to hypersonic conditions: designed by computational fluid dynamics of compressible turbulence with chemical reactions[J].热科学学报(英文版),2010,19(6):481-485,5.

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