Numerical simulation of three-dimensional supersonic flow around an aerodynamic bump
This s tudy is used to compute the primitive variables of moderate supersonic flow based on finite differen ce computational fluid dynamic methods. The problem considered deals with a three - dimensional external, inviscid ,compressible supersonic flow over a t...
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my.utm.409422017-10-08T08:32:59Z http://eprints.utm.my/id/eprint/40942/ Numerical simulation of three-dimensional supersonic flow around an aerodynamic bump A. Mohammed, Hussein Khan, Waqar Ahmed Sivasankaran, S. Mohammed, H. A. Adegun, I. K. TJ Mechanical engineering and machinery This s tudy is used to compute the primitive variables of moderate supersonic flow based on finite differen ce computational fluid dynamic methods. The problem considered deals with a three - dimensional external, inviscid ,compressible supersonic flow over a thre e - dimensional arc circular bump. In this work, Euler equation was solved using time - marching Mac Cormack’s explicit technique. The flow conditions are taken at sea level and Mach number at 1.97 . To deal with complex shape of arc circular bump the so - called “body fitted coordinate system” were considered and the algebraic methods were used to generate grids over an arc circular bump. The results showed a good agreement with other published results. 2013 Article PeerReviewed A. Mohammed, Hussein and Khan, Waqar Ahmed and Sivasankaran, S. and Mohammed, H. A. and Adegun, I. K. (2013) Numerical simulation of three-dimensional supersonic flow around an aerodynamic bump. Journal of Basic and Applied Scientific Research, 3 (7). pp. 656-666. ISSN 2090-4304 https://www.textroad.com/pdf/JBASR/J.%20Basic.%20Appl.%20Sci.%20Res.,%203(7)656-666,%202013.pdf |
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TJ Mechanical engineering and machinery A. Mohammed, Hussein Khan, Waqar Ahmed Sivasankaran, S. Mohammed, H. A. Adegun, I. K. Numerical simulation of three-dimensional supersonic flow around an aerodynamic bump |
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This s tudy is used to compute the primitive variables of moderate supersonic flow based on finite differen ce computational fluid dynamic methods. The problem considered deals with a three - dimensional external, inviscid ,compressible supersonic flow over a thre e - dimensional arc circular bump. In this work, Euler equation was solved using time - marching Mac Cormack’s explicit technique. The flow conditions are taken at sea level and Mach number at 1.97 . To deal with complex shape of arc circular bump the so - called “body fitted coordinate system” were considered and the algebraic methods were used to generate grids over an arc circular bump. The results showed a good agreement with other published results. |
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Article |
author |
A. Mohammed, Hussein Khan, Waqar Ahmed Sivasankaran, S. Mohammed, H. A. Adegun, I. K. |
author_facet |
A. Mohammed, Hussein Khan, Waqar Ahmed Sivasankaran, S. Mohammed, H. A. Adegun, I. K. |
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A. Mohammed, Hussein |
title |
Numerical simulation of three-dimensional supersonic flow around an aerodynamic bump |
title_short |
Numerical simulation of three-dimensional supersonic flow around an aerodynamic bump |
title_full |
Numerical simulation of three-dimensional supersonic flow around an aerodynamic bump |
title_fullStr |
Numerical simulation of three-dimensional supersonic flow around an aerodynamic bump |
title_full_unstemmed |
Numerical simulation of three-dimensional supersonic flow around an aerodynamic bump |
title_sort |
numerical simulation of three-dimensional supersonic flow around an aerodynamic bump |
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2013 |
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http://eprints.utm.my/id/eprint/40942/ https://www.textroad.com/pdf/JBASR/J.%20Basic.%20Appl.%20Sci.%20Res.,%203(7)656-666,%202013.pdf |
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