摘要 : The supersonic combustion scramjet in the inlet applies the shock waves compression mechanism to substitute the actual compressor from a gas turbine engine. The scramjet works with combustion of fuel through the air stream in supe... 展开
作者 | Abdulla Khamis Alhassani Mohanad Tarek Mohamed Mohammed Fares Sharul Sham Dol |
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作者单位 | |
期刊名称 | 《WSEAS Transactions on Systems》 |
总页数 | 9 |
语种/中图分类号 | 英语 / O1 |
关键词 | CFD Compression Density change Intake Mach number Pressure loss Scramjet Shockwaves |
馆藏号 | N2008EPST0010703 |