Influence of tab corner geometry on supersonic jets
The purpose of this study is to evaluate the effect of tabs having different corner geometries on the flow characteristics of a supersonic convergent-divergent (C-D) nozzle. A circular C-D nozzle of Mach 2.0 was used, and the tabs were positioned at the exit of the nozzle in diametrically opposite d...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English English |
| Published: |
Emerald
2021
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/91666/7/91666_Influence%20of%20tab%20corner%20geometry%20on%20supersonic%20jets_Scopus.pdf http://irep.iium.edu.my/91666/8/91666_Influence%20of%20tab%20corner%20geometry%20on%20supersonic%20jets.pdf http://irep.iium.edu.my/91666/ https://www.emerald.com/insight/content/doi/10.1108/AEAT-03-2021-0092/full/html |
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