Physical model of the ternary hybrid nanofluid.

Physical model of the ternary hybrid nanofluid.

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The present article describes the unsteady flow of a couple stress via a ternary hybrid nanofluid on a stretching surface with porous media. The nanofluid exhibits important properties for increasing heat transmission, and it is widely used in manufacturing and industrial applications. The basic similarity equations have been discovered to accommod...

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... the present work, we use nonNewtonian coupling. Moreover, it should be noted that the water containing spherical aluminum oxide, cylindrical single wall CNT, and platelet graphene nanoparticles, as shown in Figure 1, is transported. Table 1 shows the thermal characteristics of these three nanofluids. ...
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... ternary hybrid nanoparticles within the nanofluid increase as the volume fraction of the nanoparticles increases, allowing for an increased area for improved heat conduction. As can be seen in Figure 11, this raises the velocity of the nanofluid. Figure 12 shows the impact of ( ) θ η on η for various values of Λ for the stretching surface. ...
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... can be seen in Figure 11, this raises the velocity of the nanofluid. Figure 12 shows the impact of ( ) θ η on η for various values of Λ for the stretching surface. ( ) θ η decreases with an increase the value of Λ , and it is observed that the boundary layer thickness also reduces in the stretching surface. ...
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... ) θ η decreases with an increase the value of Λ , and it is observed that the boundary layer thickness also reduces in the stretching surface. Figure 13 indicates the impact of ( ) θ η on η for various values of the Biot number for the stretching case. Here, it seen that ( ) θ η decreases as the value of the Biot number increases. ...
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... performance of nanofluids is affected by both the drop in particle volume fraction and the increase in temperature in the flow pattern. Figure 14 show the temperature distribution ( ) θ η versus the similarity variable η for various values of the mass transpiration Vc for the stretching surface. This means that the thickness of the thermal boundary layer under suction is thinner than under blowing. ...
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... means that the thickness of the thermal boundary layer under suction is thinner than under blowing. Figure 15 show the temperature distribution ( ) θ η versus the similarity variable η for various values of the thermal radiation NR for the stretching surface. Thermal radiation, therefore, increases the thermal diffusivity of nanofluids; for emerging radiation parameter values, heat will be added to the regime, and temperatures will rise as a result. ...
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... has the effect of dampening or enhancing heat transmission in a linear manner. Figure 16a,b show the streamline flow patterns for suction and injection situations, respectively. For suction and injection scenarios, we look at different line patterns. ...
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... suction and injection scenarios, we look at different line patterns. The streamline flow pattern for the stretched boundaries is shown in Figure 16a,b for varied levels of mass transpiration Vc while other parameters remain constant. When wall suction occurs at specific locations, as predicted by the physical theory, the flow field becomes regularized. ...
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... the other hand, blowing (flow injection) eliminates the streamline in the circular shape. Figure 17 indicates the effect of the skin friction coefficient on the stretching/shrinking surface λ as a function of couple stress Λ , respectively. ...
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... it is noticed that the couple stress parameter is the reciprocal of thickness decreasing of the boundary layer occurs via the same process. While skin friction is linearly proportional to the thickness of the boundary layer, it is estimated to have an inverse proportionality λ , as depicted in Figure 17. In addition, upward pulling couple stress parameters will draw fluid toward the negative y direction and reduce skin friction. ...
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... thickness of the boundary layer will decrease when the suction parameter, which measures the strength of wall suction, is increased, and as a result, the gradient of the velocity on the wall will also increase. This impact will enhance skin friction, as shown in Figure 17. Figure 18 shows the effect of the skin friction coefficient on couple stress Λ as a function of the stretching/shrinking surface λ , respectively. ...
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... impact will enhance skin friction, as shown in Figure 17. Figure 18 shows the effect of the skin friction coefficient on couple stress Λ as a function of the stretching/shrinking surface λ , respectively. Here, it should be noted that the process of the decrease of the boundary layer's thickness and the stretching/shrinking surface parameter are the same. ...
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... it should be noted that the process of the decrease of the boundary layer's thickness and the stretching/shrinking surface parameter are the same. Skin friction is thought to have an inverse relationship with boundary layer thickness, as shown in Figure 18, even though the two are linearly proportional λ . Additionally, fluid will be drawn toward the negative y direction, and the skin friction will be decreased by the upward pulling couple stress parameters. ...
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... suction parameter, which gauges the strength of the wall suction, causes a reduction in the thickness of the boundary layer, which causes an increase in the gradient of velocity on the wall. The increase in skin friction caused by this collision is depicted in Figure 18. ...

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