Couette-Poiseuille flow based non-linear flow over a square cylinder near plane wall
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作者:
Bhatt, Rajesh
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Harbin Inst Technol, Shenzhen Grad Sch, Inst Turbulence Noise Vibrat Interact & Control, Shenzhen, Peoples R ChinaHarbin Inst Technol, Shenzhen Grad Sch, Inst Turbulence Noise Vibrat Interact & Control, Shenzhen, Peoples R China
Bhatt, Rajesh
[1
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Maiti, Dilip K.
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Vidyasagar Univ, Dept Appl Math Oceanol & Comp Programming, Midnapore 721102, IndiaHarbin Inst Technol, Shenzhen Grad Sch, Inst Turbulence Noise Vibrat Interact & Control, Shenzhen, Peoples R China
Maiti, Dilip K.
[2
]
Alam, Md. Mahbub
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Harbin Inst Technol, Shenzhen Grad Sch, Inst Turbulence Noise Vibrat Interact & Control, Shenzhen, Peoples R ChinaHarbin Inst Technol, Shenzhen Grad Sch, Inst Turbulence Noise Vibrat Interact & Control, Shenzhen, Peoples R China
Alam, Md. Mahbub
[1
]
Rehman, S.
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King Fahd Univ Petr & Minerals, Res Inst, Ctr Engn Res, Dhahran 31261, Saudi ArabiaHarbin Inst Technol, Shenzhen Grad Sch, Inst Turbulence Noise Vibrat Interact & Control, Shenzhen, Peoples R China
Rehman, S.
[3
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机构:
[1] Harbin Inst Technol, Shenzhen Grad Sch, Inst Turbulence Noise Vibrat Interact & Control, Shenzhen, Peoples R China
[2] Vidyasagar Univ, Dept Appl Math Oceanol & Comp Programming, Midnapore 721102, India
[3] King Fahd Univ Petr & Minerals, Res Inst, Ctr Engn Res, Dhahran 31261, Saudi Arabia
A numerical study on the flow over a square cylinder in the vicinity of a wall is conducted for different Couette-Poiseuille-based non-uniform flow with the non-dimensional pressure gradient P varying from 0 to 5. The non dimensional gap ratio L (=H*/a*) is changed from 0.1 to 2, where H* is gap height between the cylinder and wall, and a* is the cylinder width. The governing equations are solved numerically through finite volume method based on SIMPLE algorithm on a staggered grid system. Both P and L have a substantial influence on the flow structure, time-mean drag coefficient (C) over bar (D), fluctuating (rms) lift coefficient (C-L'), and Strouhal number St. The changes in P and L leads to four distinct flow regimes (I, II, III and IV). Following the flow structure change, the (C) over bar (D), C-L' and St all vary greatly with the change in L and/or P. The (C) over bar (D) and C-L' both grow with increasing P and/or L. The St increases with P for a given L, being less sensitive to L for a smaller P (< 2) and more sensitive to L for a larger P (> 2). A strong relationship is observed between the flow regimes and the values of (C) over bar (D), C-L' and St. An increase in P affects the pressure distribution more on the top surface than on bottom surface while an increase in L does the opposite.