Computational analysis of thrust generated by converging-diverging nozzle at different diverging angles
This study investigated the pressure rise characteristics of a shock train contained within a duct representative of a supersonic combustion ramjet (scramjet) isolator. The simulated isolator consisted of a constant area (25 mm by 30 mm) rectangular duct back-pressured by a triangular-shaped wedge...
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| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | en |
| Published: |
Semarak Ilmu Publishing
2025
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/119211/1/ARNHT29_N1_P102_128.pdf http://irep.iium.edu.my/119211/ https://semarakilmu.com.my/journals/index.php/arnht/ |
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