Performance Prediction of Internal Compression Supersonic Air Intake at Range of Mach Numbers (1.1 -1.5)
<span>In this research a numerical investigation on a supersonic air intake was done. The aim of this <span>work is to investigate a variable geometry of cross-section area for supersonic air intake at range <span>(1.1 -1.5) Mach number, to get a maximum pressure recovery. In this...
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| Format: | Article |
| Language: | English |
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Tikrit University
2017-12-01
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| Series: | Tikrit Journal of Engineering Sciences |
| Subjects: | |
| Online Access: | http://www.tj-es.com/ojs/index.php/tjes/article/view/641 |