An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle
This paper presents the results of an experimental investigation conducted at supersonic Mach number of 1.25 through a converging–diverging nozzle for diameter-ratio of 1.6. The experiments were conducted at different level of expansion viz. for correctly expanded and under expanded cases and, for...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | en |
| Published: |
UNIV LAGOS
2016
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/51373/1/our_paper.pdf http://irep.iium.edu.my/51373/ http://jsrad.org/wp-content/2016/Issue%205,%202016/1j.pdf |
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