Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles
Computational Fluid Dynamics simulations were carried out using ANSYS FLUENT for suddenly expanded flow through the convergent-divergent nozzle and a suddenly expanded duct. The Length-to-Diameter ratio of 10 for the duct was used in the analysis. Also, an Area Ratio between CD Nozzle exit area and...
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Blue Eyes Intelligence Engineering & Sciences Publication
2019
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| オンライン･アクセス: | http://irep.iium.edu.my/71059/7/71059%20Investigation%20of%20the%20effects%20of%20nozzle%20exit%20mach%20number.pdf http://irep.iium.edu.my/71059/8/71059%20Investigation%20of%20the%20effects%20of%20nozzle%20exit%20mach%20number%20SCOPUS.pdf http://irep.iium.edu.my/71059/ https://www.ijeat.org/wp-content/uploads/papers/v8i3/C5986028319.pdf |
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my.iium.irep.710592019-07-12T07:42:23Z http://irep.iium.edu.my/71059/ Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles Khan, Sher Afghan Mohiuddin, M Saleel, Ahmad C G M, Fharukh TJ751 Miscellaneous motors and engines. Including gas, gasoline, diesel Computational Fluid Dynamics simulations were carried out using ANSYS FLUENT for suddenly expanded flow through the convergent-divergent nozzle and a suddenly expanded duct. The Length-to-Diameter ratio of 10 for the duct was used in the analysis. Also, an Area Ratio between CD Nozzle exit area and Duct Area was used to be 1.6. The effects of Nozzle Exit Mach number and the Nozzle Pressure Ratios were evaluated by conducting the simulations for Nozzle Exit Mach numbers: 1.87, 2.25 and 2.58. For each Mach number then, Nozzle Pressure Ratios of 3, 5, 7, 9, and 11 were set respectively. Making a total of 15 cases. All the cases were simulated using the k-ω turbulence model. Simulated results agree with the experimental data. From the analysis, it is clear that the Nozzle Exit Mach number and Nozzle Pressure Ratio have a direct effect on the expanded flow exiting the nozzle. Blue Eyes Intelligence Engineering & Sciences Publication 2019-02 Article PeerReviewed application/pdf en http://irep.iium.edu.my/71059/7/71059%20Investigation%20of%20the%20effects%20of%20nozzle%20exit%20mach%20number.pdf application/pdf en http://irep.iium.edu.my/71059/8/71059%20Investigation%20of%20the%20effects%20of%20nozzle%20exit%20mach%20number%20SCOPUS.pdf Khan, Sher Afghan and Mohiuddin, M and Saleel, Ahmad C and G M, Fharukh (2019) Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles. International Journal of Engineering and Advanced Technology (IJEAT), 8 (3). pp. 570-578. https://www.ijeat.org/wp-content/uploads/papers/v8i3/C5986028319.pdf |
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Universiti Islam Antarabangsa Malaysia |
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Malaysia |
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| language |
English English |
| topic |
TJ751 Miscellaneous motors and engines. Including gas, gasoline, diesel |
| spellingShingle |
TJ751 Miscellaneous motors and engines. Including gas, gasoline, diesel Khan, Sher Afghan Mohiuddin, M Saleel, Ahmad C G M, Fharukh Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles |
| description |
Computational Fluid Dynamics simulations were carried out using ANSYS FLUENT for suddenly expanded flow through the convergent-divergent nozzle and a suddenly expanded duct. The Length-to-Diameter ratio of 10 for the duct was used in the analysis. Also, an Area Ratio between CD Nozzle exit area and Duct Area was used to be 1.6. The effects of Nozzle Exit Mach number and the Nozzle Pressure Ratios were evaluated by conducting the simulations for Nozzle Exit Mach numbers: 1.87, 2.25 and 2.58. For each Mach number then, Nozzle Pressure Ratios of 3, 5, 7, 9, and 11 were set respectively. Making a total of 15 cases. All the cases were simulated using the k-ω turbulence model. Simulated results agree with the experimental data. From the analysis, it is clear that the Nozzle Exit Mach number and Nozzle Pressure Ratio have a direct effect on the expanded flow exiting the nozzle. |
| format |
Article |
| author |
Khan, Sher Afghan Mohiuddin, M Saleel, Ahmad C G M, Fharukh |
| author_facet |
Khan, Sher Afghan Mohiuddin, M Saleel, Ahmad C G M, Fharukh |
| author_sort |
Khan, Sher Afghan |
| title |
Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles |
| title_short |
Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles |
| title_full |
Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles |
| title_fullStr |
Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles |
| title_full_unstemmed |
Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles |
| title_sort |
investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles |
| publisher |
Blue Eyes Intelligence Engineering & Sciences Publication |
| publishDate |
2019 |
| url |
http://irep.iium.edu.my/71059/7/71059%20Investigation%20of%20the%20effects%20of%20nozzle%20exit%20mach%20number.pdf http://irep.iium.edu.my/71059/8/71059%20Investigation%20of%20the%20effects%20of%20nozzle%20exit%20mach%20number%20SCOPUS.pdf http://irep.iium.edu.my/71059/ https://www.ijeat.org/wp-content/uploads/papers/v8i3/C5986028319.pdf |
| _version_ |
1643619962132103168 |
| score |
13.250246 |