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Problem 7.2 This is an external free convection problem over a vertical plate. The Rayleigh number should be computed to determine if the flow is laminar or turbulent. The solution for laminar flow is given in Section 7.4 For laminar flow, Fig.7.2 gives the viscous boundary layer thickness and Fig. 7.3 gives the thermal boundary layer thickness t . Newton’s law of cooling gives the heat transfer rate. Equation (7.23) gives the average heat transfer coefficient h . (vii) The fluid is water. Problem 7.3 This is an external free convection problem for flow over a vertical plate. Laminar flow solution for temperature distribution for a plate at uniform surface temperature is given in Fig. 7.3 . The dimensionless temperature gradient at the surface is given in Table 7.1. The solution depends on the Prandtl number. Problem 7.4 This is a free convection problem. Heat is lost from the door to the surroundings by free convection and radiation. To determine the rate of heat loss, the door can by modeled as a vertical plate losing heat by free convection to an ambient air. As a first approximation, radiation can be neglected. Newton’s law of cooling gives the rate of heat transfer. The Rayleigh number should be computed to determine if the flow is laminar or turbulent. For laminar flow the solution of Section 7.4 is applicable. Problem 7.5 This is a free convection and radiation problem. The geometry is a vertical plate. Surface temperature is uniform. Newton’s law of cooling gives convection heat transfer rate while Stefan-Boltzmann law gives radiation heat transfer rate. The Rayleigh number should be computed to determine if the flow is laminar or turbulent. For laminar flow the solution of Section 7.4 is applicable. Since radiation heat transfer is considered in this problem, all temperatures should be expressed Problem 7.6 This is a free convection problem. The power dissipated in the electronic package is transferred to the ambient fluid by free convection. As the power is increased, surface temperature increases. The maximum power dissipated corresponds to the maximum allowable surface temperature. Surface temperature is related to surface heat transfer by Newton’s law of cooling. The problem can be modeled as free convection over a vertical plate. The Rayleigh number should be computed to determine if the flow is laminar or turbulent. For laminar flow the solution of Section 7.4 is applicable. The fluid is air. Problem 7.7 This is a free convection problem. The power dissipated in the electronic package is transferred to the ambient fluid by free convection. As the power is increased, surface temperature increases. The maximum power dissipated corresponds to the maximum allowable surface temperature. Surface temperature is related to surface heat transfer by Newton’s law of cooling. The problem can be modeled as free convection over a vertical plate. The Rayleigh number should be computed to determine if the flow is laminar or turbulent. For laminar flow the solution of Section 7.4 is applicable. The fluid is water. Problem 7.8 This is a free convection problem. The surface is maintained at uniform temperature. Newton’s law of cooling determines the heat transfer rate. Heat transfer rate depends on the heat transfer coefficient. The heat transfer coefficient decreases with distance from the leading edge of the plate. The width of each triangle changes with distance from the leading edge. For laminar flow the solution of Section 7.4 is applicable. Problem 7.9 This is a free convection problem over a vertical plate. The surface is maintained at uniform temperature. Local heat flux is determined by Newton’s law of cooling. Heat flux depends on the local heat transfer coefficient Free convection heat transfer coefficient for a vertical plate decreases with distance from the leading edge. Thus, the flux also decreases. The Rayleigh number should be computed to determine if the flow is laminar or turbulent. For Laminar flow the solution of Section 7.4 is applicable. The fluid is air. Problem 7.10 This is a free convection problem over a vertical plate. The power dissipated in the chips is transferred to the air by free convection. This problem can be modeled as free convection over a vertical plate with constant surface heat flux. Surface temperature increases as the distance from the leading edge is increased. Thus, the maximum surface temperature occurs at the top end of the plate (trailing end). The Rayleigh number should be computed to determine if the flow is laminar or turbulent. For laminar flow the analysis of Section 7.5 gives surface temperature distribution. The fluid is air. Properties depend on the average surface temperature Ts . Since Ts is unknown, the problem must be solved by trail and error. Problem 7.11 This is a free convection problem over a vertical plate. The power dissipated in the chips is transferred to the air by free convection This problem can be modeled as free convection over a vertical plate with constant surface heat flux. Surface temperature increases as the distance from the leading edge is increased. Thus, the maximum surface temperature occurs at the top end of the plate (trailing end). The Rayleigh number should be computed to determine if the flow is laminar or turbulent. For laminar flow the analysis of Section 7.5 gives surface temperature distribution. The fluid is air. Properties depend on the average surface temperature Ts . Since Ts is unknown, the problem must be solved by trail and error. Problem 7.12 This is a free convection problem over a vertical plate at uniform surface temperature. In general, to determine the Nusselt number it is necessary to determine the velocity and temperature distribution. The integral method can be used to determine the velocity and temperature distribution. Application of the integral method reduces to determining the velocity and temperature boundary layer thickness. Problem 7.13 This is a free convection problem over a vertical plate at uniform surface heat flux. In general, to determine the Nusselt number it is necessary to determine the velocity and temperature distribution. The integral method can be used to determine the velocity and temperature distribution. Application of the integral method reduces to determining the velocity and temperature boundary layer thickness.