Combined Effect Of Incidence - Forebody Angles on the Flow Structure Inside Spiked Supersonic Intakes
A high static pressure at the inlet face and minimal total pressure loss at the intake entry are required for an efficient operation of the spiked supersonic jet engines. The turning (Forebody) angles are optimized for a maximum total pressure recovery at the intake entry for the design Mach number...
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| Main Authors: | , |
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| Format: | Conference or Workshop Item |
| Published: |
2008
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| Subjects: | |
| Online Access: | http://eprints.utp.edu.my/4196/1/AMME_paper_combined_effect_1_page_-new.pdf http://eprints.utp.edu.my/4196/ |
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