Performance Prediction of Internal Compression Supersonic Air Intake at Range of Mach Numbers (1.1-1.5)
In this research, a numerical investigation on a supersonic air intake was done. The aim of this work is to investigate a variable geometry of cross-section area for supersonic air intake at range (1.1-1.5) Mach number, to get a maximum pressure recovery. In this work, the flow starts with a normal...
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| Format: | Article |
| Language: | English |
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Tikrit University
2016-09-01
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| Series: | Tikrit Journal of Engineering Sciences |
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| Online Access: | http://tj-es.com/vol23no3pa4/ |