| Title: |
Numerical studies of Newtonian and viscoelastic fluids
|
| Author: | |
| Document Type: |
Dissertation
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| Department: |
Department of Mechanical Engineering
|
| Degree: |
Doctor of Philosophy
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| Major: |
Mechanical Engineering
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| Advisory Committee: |
Singh, Pushpendra
Chen, Rong-Yaw
Aubry, N.
Narh, Kwabena A.
Tilley, Burt S.
|
| Thesis Date: |
2001, January
|
| Keywords: |
Viscoelastic Fluids
Porous Media Flows
Four to One Contraction
Flow Past An Air Foil
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| Availability: |
Unrestricted
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| Abstract: |
The direct numerical simulation (DNS) approach is used to understand the flow behavior of Newtonian and viscoelastic fluids in porous materials, four-to-one contraction and the flow of a Newtonian fluid past an airfoil. In simulations the viscoelastic fluid is modeled by the finitely extensible nonlinear elastic (FENE) dumbbell and Oldroyd-B models. The finite element method (FEM) is used to discretize the flow domain. The DNS results show that the permeability of a periodic porous medium depends on the wavelength used for arranging particles in the direction of flow. Specifically, it is shown that for a given particle size and porosity the permeability varies when the distance between particles in the flow direction is changed. The permeability is locally minimum for kD [approximately equal to] 7.7 and locally maximum for kD [approximately equal to] 5.0; where k is the wave number and D the diameter. A similar behavior holds for a viscoelastic fluid, except that the variation of permeability with kD is larger than for the Newtonian case. For flow in the four-to-one contraction, it is found that the stress near the 3π/2 comer is singular and that the singularity is stronger than for a Newtonian liquid. In the region away from the walls, the stress varies as r -0.47 and near the walls it varies as r -0.61. Since the singularity is integrable, the flow away from the comer is not effected [sic] when the flow around the comer is resolved by using a radial mesh with sufficient resolution in the tangential direction at the comer. The DNS approach is also used to demonstrate that the boundary layer separation on the upper surface of the airfoil can be suppressed by placing injection and suction regions on the upper surface. The simulations are performed for Re ≤ [less than or equal too] 500 and angle of attack up to 40°. Analysis of numerical results shows that the pressure contribution to drag decreases when the boundary layer separation is avoided. The viscous contribution to drag, however, increases and thus there is only a negligible decrease in the total drag for Re ≤ [less than or equal too] 500. Another beneficial effect of suction and injection is that the pressure contribution to the lift increases and the stall is avoided. |
| Complete Thesis: |
njit-etd2001-048
(167 pages ~ 5,381 KB pdf)
|
| Download by Chapters: |
Front
Matter (Title Page, Abstract, Table
of Contents, etc. ~ 17 pages ~ 596 KB pdf)
Chapter
1: Introduction (14 pages ~ 643 KB
pdf)
Chapter
2: Governing Equations (4 pages ~ 127
KB pdf)
Chapter
3: Numerical Method (9 pages ~ 292
KB pdf)
Chapter
4: Permeability of Periodic Porous Media (20
pages ~ 563 KB pdf)
Chapter
5: Viscoelastic Porous Media Flows (20
pages ~ 733 KB pdf)
Chapter
6: Viscoelastic Flow ina Four-to-One Contraction (46
pages ~ 1,325 KB pdf)
Chapter
7: Numerical Studies of Boundary Layer Control (38
pages ~ 953 KB pdf)
References
(7 pages ~ 382 KB pdf)
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