Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56
Airflow from convergent-divergent axisymmetric nozzles expanded into circular duct of higher area were studied experimentally, with the main focus on the flow development in the duct. The flow parameters considered in this investigation are the Mach number at the nozzle exit and the level of expansi...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
IOSR journals
2016
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/54294/ http://irep.iium.edu.my/54294/ http://irep.iium.edu.my/54294/1/Musavir.pdf |