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Steady flow of a power law fluid through a tapered non-symmetric stenotic tube


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Fig. 1

Geometry of non-symmetric stenotic artery.
Geometry of non-symmetric stenotic artery.

Fig. 2

Stenotic tapered artery for different taper angles.
Stenotic tapered artery for different taper angles.

Fig. 3

Velocity variation for F=2, δ=0.4, n=2, a=0.2, b=0.4.
Velocity variation for F=2, δ=0.4, n=2, a=0.2, b=0.4.

Fig. 4

Velocity variation for F=2, n=2, a=0.2, b=0.4, m=1.1.
Velocity variation for F=2, n=2, a=0.2, b=0.4, m=1.1.

Fig. 5

Velocity variation for F=2,δ =0.2, n=2, a=0.2, b=0.4, m=1.
Velocity variation for F=2,δ =0.2, n=2, a=0.2, b=0.4, m=1.

Fig. 6

Velocity variation for F=2, δ=0.4, a=0.2, b=0.4, m=1.1.
Velocity variation for F=2, δ=0.4, a=0.2, b=0.4, m=1.1.

Fig. 7

Wall shear stress variation for F=1, δ=0.2, a=0.2, b=0.4, m=1.
Wall shear stress variation for F=1, δ=0.2, a=0.2, b=0.4, m=1.

Fig. 8

Wall shear stress variation for F=1, L=1, a=0.2, b=0.4, m=1.
Wall shear stress variation for F=1, L=1, a=0.2, b=0.4, m=1.

Fig. 9

Wall shear stress variation for F=1, L=1, a=0.2, b=0.4,δ=0.4.
Wall shear stress variation for F=1, L=1, a=0.2, b=0.4,δ=0.4.

Fig. 10

Wall shear stress variation for F=1, L=1, a=0.2, b=0.4,δ=0.4.
Wall shear stress variation for F=1, L=1, a=0.2, b=0.4,δ=0.4.

Fig. 11

Resistance impedance for F=0.6, L=1, a=0.2, b=0.4, m=2.
Resistance impedance for F=0.6, L=1, a=0.2, b=0.4, m=2.

Fig. 12

Resistance impedance for F=0.6, L=1, a=0.2, b=0.4, n=2.
Resistance impedance for F=0.6, L=1, a=0.2, b=0.4, n=2.

Fig. 13

Resistance impedance for F=0.6, L=1, a=0.2, b=0.4, m=1.2, n=2.
Resistance impedance for F=0.6, L=1, a=0.2, b=0.4, m=1.2, n=2.

Fig. 14

Shear stress at stenotic throat for F=0.2.
Shear stress at stenotic throat for F=0.2.

Fig. 15

Shear stress at stenotic throat for m=2.
Shear stress at stenotic throat for m=2.
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