Performance prediction procedures of the supersonic spiked intakes
The supersonic flow approaching the intake of a supersonic aero engine must be brought to subsonic state before reaching the compressor face stage. The velocity reduction is combined with reduction in the total pressure of the flow which is not preferred by the designer of the supersonic gas turbine...
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| Main Authors: | , , |
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| Format: | Citation Index Journal |
| Published: |
ANSInet
2011
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| Subjects: | |
| Online Access: | http://eprints.utp.edu.my/7359/1/224-235.pdf http://www.scimagojr.com http://eprints.utp.edu.my/7359/ |
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