Effect of cavities in suddenly expanded flow at supersonic mach number
The contribution from the base drag due to the sub-atmospheric pressure is significant. It can be more than two-thirds of the net drag. There is a need to increase the base pressure and hence decrease the base drag. This research examines the effect of Mach number on base pressure. To accomplish thi...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English English |
| Published: |
Semarak Ilmu Publishing
2021
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/92639/7/92639_Effect%20of%20cavities%20in%20suddenly%20expanded%20flow%20at%20supersonic%20mach%20number.pdf http://irep.iium.edu.my/92639/13/92639_Effect%20of%20cavities%20in%20suddenly%20expanded%20flow%20at%20supersonic%20mach%20number_Scopus.pdf http://irep.iium.edu.my/92639/ https://semarakilmu.com.my/journals/index.php/CFD_Letters/article/view/5 https://doi.org/10.37934/cfdl.13.9.5771 |
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http://irep.iium.edu.my/92639/7/92639_Effect%20of%20cavities%20in%20suddenly%20expanded%20flow%20at%20supersonic%20mach%20number.pdfhttp://irep.iium.edu.my/92639/13/92639_Effect%20of%20cavities%20in%20suddenly%20expanded%20flow%20at%20supersonic%20mach%20number_Scopus.pdf
http://irep.iium.edu.my/92639/
https://semarakilmu.com.my/journals/index.php/CFD_Letters/article/view/5
https://doi.org/10.37934/cfdl.13.9.5771