Fig 1.
Flow configuration and coordinate system.
Table 1.
Definitions of physical parameters.
Table 2.
Mesh analysis or grid independence test for Pr = 7.0, γ = 1.0, Sc = 10.0, ε = 1.0, Nt = 0.4, and Nb = 0.2 at X = π/4.
Table 3.
Validation of numerical model; comparison of with the results of Sparrow & Gregg [26], γ = 0.0, Sc = 0.0, ε = 0.0, Nt = 0.0, and Nb = 0.0 at X = π/2.
Table 4.
Definitions of physical parameters appeared in the Plume region-III.
Fig 2.
Variation of (a) U (b) θ and (c) ϕ for γ = 0.1, 0.5, when ε = 10.0, Nb = 0.4, Nt = 0.2, Sc = 0.5 and Pr = 7.0.
Fig 3.
Variation of (a) U (b) θ and (c) ϕ for ε = 1.0, 10.0, when γ = 10.0, Nb = 0.4, Nt = 0.2, Sc = 0.5 and Pr = 7.0.
Fig 4.
Variation of (a) U (b) θ and (c) ϕ for Nt = 0.2, 0.6, when γ = 10.0, Nb = 0.4, Sc = 0.5, ε = 1.0 and Pr = 7.0.
Fig 5.
Variation of (a) U (b) θ and (c) ϕ for Nb = 0.1, 10.0, when γ = 10.0, Nt = 0.2, Sc = 0.5, ε = 1.0 and Pr = 7.0.
Fig 6.
Variation of (a) U (b) θ and (c) φ for Nb = 0.1, 10.0, when γ = 10.0, Nb = 0.2, Sc = 0.5, ε = 1.0 and Pr = 7.0.
Table 5.
Variation of (a)Skin friction , (b) Heat Transer
and (c) Mass Transfer
for ε = 1.0, Pr = 7.0, Sc = 10.0, Nt = 10.0, and Nb = 1.0.
Table 6.
Variation of (a)Skin friction , (b)Heat Transfer
and (c) Mass Transfer
for γ = 1.0, Pr = 7.0, Sc = 10.0, Nt = 0.4, and Nb = 0.2.
Table 7.
Variation of (a)Skin friction , (b)Heat Transfer
and (c) Mass Transfer
for γ = 10.0, Pr = 7.0, ε = 1.0, Nt = 0.4, and Nb = 0.2.
Fig 7.
Variation of (a) W (b) θ and (c) ϕ for different value of γ when ε = 10.0, Nb = 0.4, ε = 10.0, Sc = 0.5 and Pr = 7.0.
Table 8.
Variation of (a)Skin friction , (b)Heat Transfer
and (c) Mass Transfer
for γ = 10.0, Pr = 7.0, ε = 1.0, Nt = 0.4, and Nb = 0.2.
Table 9.
Variation of (a) Skin friction , (b) Heat Transfer
and (c) Mass Transfer
for γ = 50.0, Pr = 7.0, ε = 10.0, Nt = 0.5, and Nb = 0.6.