Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers
The experimental analysis of base pressure in a high-speed compressible flow is carried out. The flow is made to expand abruptly from the nozzle into an enlarged duct at fifteen sonic and supersonic Mach numbers. The analysis is made for variation in the nozzle pressure ratio (NPR), length to diamet...
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| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English English English |
| Published: |
AIP Publishing
2020
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/83245/1/83245_Investigation%20and%20back-propagation%20modeling_ft.pdf http://irep.iium.edu.my/83245/7/83245_Investigation%20and%20back-propagation%20modeling_SCOPUS.pdf http://irep.iium.edu.my/83245/8/83245_Investigation%20and%20back-propagation%20modeling_WOS.pdf http://irep.iium.edu.my/83245/ https://aip.scitation.org/doi/10.1063/5.0022015 https://doi.org/10.1063/5.0022015 |
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| Institution: | Universiti Islam Antarabangsa Malaysia |
| Language: | English English English |