Supersonic blowdown wind tunnel control using ABC optimized PID controller
Supersonic blowdown wind tunnels enable the testing of aircraft prototypes in the Mach 1.2 to 5 range, but these tunnels allow very limited test times due to their structure. In addition, once the wind tunnel system starts operating, the pressure in the tank where the air is stored changes constantl...
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| Principais autores: | , , , , , |
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| Format: | Artigo |
| Sprog: | Inglês |
| Udgivet: |
Selçuk Üniversitesi
2025-06-01
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| Serier: | International Journal of Aeronautics and Astronautics |
| Fag: | |
| Online adgang: | https://dergipark.org.tr/tr/download/article-file/4471773 |
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