Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers
In this investigation the flow field has been computed by the numerical approach using Computational Fluid Dynamics (CFD) Analysis to investigate the efficacy of the supersonic Mach numbers due to the flow from supersonic nozzle exhausted in a larger circular duct and the corresponding thrust force...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
Elsevier
2018
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/66581/ http://irep.iium.edu.my/66581/ http://irep.iium.edu.my/66581/ http://irep.iium.edu.my/66581/1/66581_Optimization%20of%20area%20ratio%20and%20thrust.pdf http://irep.iium.edu.my/66581/7/66581%20Optimization%20of%20area%20ratio%20and%20thrust%20in%20suddenly%20expanded%20flow%20at%20supersonic%20SCOPUS.pdf |
Internet
http://irep.iium.edu.my/66581/http://irep.iium.edu.my/66581/
http://irep.iium.edu.my/66581/
http://irep.iium.edu.my/66581/1/66581_Optimization%20of%20area%20ratio%20and%20thrust.pdf
http://irep.iium.edu.my/66581/7/66581%20Optimization%20of%20area%20ratio%20and%20thrust%20in%20suddenly%20expanded%20flow%20at%20supersonic%20SCOPUS.pdf