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Heat Transfer Project 1 MECH 4315 Instructor: Evgeny Shafirovich 04/06/2015 Group 4 Irma Edith Duran Reyes Joao De Rezende Martins Lucas Da Silva Rigobello

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  • Heat Transfer Project 1 MECH 4315 Instructor: Evgeny Shafirovich 04/06/2015 Group 4 Irma Edith Duran Reyes Joao De Rezende Martins Lucas Da Silva Rigobello

  • Natural convection of the heat plate First, It is calculated the heat transfer for the heater by itself. It is the rate of heat transfer for a horizontal hot plate by natural convection. In all calculations the gravity is constant = 9.81 / and the assumptions are: room temperature at 24C, constant temperature at fins and base, vertical positions of fins. Data Room temperature: = 24 Surface Temperature: = 85 Length: = 2.54 Width: = 7.62 Calculation process Surface Area: = = 1.9354810 !! ! Perimeter: = 2 + = 0.2032 Film Temperature: = !"!!! = 54.5 Then using the film temperature, the follow numbers were taken from the Table A-15 (Properties of air at 1 atm pressure) from the textbook:

    Kinematic viscosity: = 1.842110!! !!! Prandtl Number: = 0.72163 Thermal diffusivity: = 0.027678 Volume expansion coefficient: = !!"!!"# = 0.0031 !! Characteristic Length: = !"! = 0.0095 Rayleigh Number: ! = !! !"!! !!!!! = 3.357910! Nusselt Number: = 0.54!!! = 4.1107 Heat transfer coefficient: = !"!!" = 11.9449 !! ! Heat transfer rate: = = 1.4103

    Heat Sink Design Now, to project the heat sink it is supposed that the heat sink should be able to dissipate the same amount of heat of the initial hot plate, but in a low temperature (70 ). It is only possible because of the larger surface area than the actual plate, which the heat sink is going to have. So, by calculating the optimum space between each two fins, it is possible to have an initial idea to choose some close or appropriate number desired for the actual space between each two fins. As well, it can be assumed some value for the fin high that goes from 2.54>H>0 (cm). Then it is calculated the thickness of each fin and the needed number of fins to dissipate the same amount of heat as the hot plate. For this, a Matlab code was made

  • to help in the calculation and interaction to find the desired parameters that would make sense for the project. Data Room temperature: = 24 Contact Temperature: = 70 Length: = 2.5410! Width: = 7.6210! High: = 2.5410! Parameters

    Space between each two fins: = 5.2 High of the fin: = 13.0 Heat Sink calculations Firs, to find the temperature at the base of the fin, it is need to consider the conduction of heat, the total dissipated by the plate, through the material from the contact with the heater to base of the fin. Distance from the contact to the fin base: = = 0.0124 Thermal conductivity of the material (Aluminum): = 173 !! ! Thermal Resistance: = !!"#!" = 0.037 !! Temperature at the base of the fin: = = 69.9478 The second part of the calculation is the part referred to the fins calculation. Film Temperature: = !"!!! = 46.9739 Then using the film temperature, the follow numbers are taken from the Table A-15 (Properties of air at 1 atm pressure) from the textbook:

    Kinematic viscosity: = 1.769210!! !!! Prandtl Number: = 0.72332 Thermal diffusivity: = 0.02735 Volume expansion coefficient: = !!"!!!" = 0.0031 !! Calculating the Optimum Space between each two fins: Rayleigh Number: ! = !! !"!! !!!! = 5.334110! Optimum Space between each two fins: = 2.714 !!"!!.!" = 4.5361 (So the chosen for the math is reasonable since it is bigger than ) Now considering the from the parameters, the calculation can follows as:

  • Rayleigh Number: ! = !! !"!! !!!! = 457.7260 Nusselt Number: = !"#!"!!! ! + !.!"#!"!!! !.! !!.! = 1.6612 Heat transfer coefficient: = !"!! = 8.7371 !! ! Number of fins: = !! !!! !"!! = 5.3194 Thickness of each fin: = 9.125 Heat transfer in the side faces of the base

    Surface: = = 0.000944 ! Perimeter: = 2 + = 0.1772 Film Temperature: = !"!!! = 46 Then using the film temperature, the follow numbers were taken from the Table A-15 (Properties of air at 1 atm pressure) from the textbook: Kinematic viscosity: = 1.79810 5 !!! Prandtl Number: = 0.7228 Thermal diffusivity: = 0.02735 Volume expansion coefficient: = !!"!!"# = 0.00313 !! Characteristic Length: = !"! = 0.005327 Rayleigh Number: ! = !! !"!! !!!!! = 476.89 Nusselt Number: = 0.54!!! = 9.8775 Heat transfer coefficient: = !"!!! = 2.52 !! ! Heat transfer rate: = = 0.109579 = ! = 1.3007

    a) Figure a) CAD model b) final heat sink b)

  • Matlab Code g=9.81; %Hot Plate------------------------------------------ Ts=85; T=24; L=2.54e-2; W=7.62e-2; As=W*L Lc=As/(2*(W+L)) tf=(Ts+T)/2 kv=1.8421e-5; Pr=0.72163; k=0.027678; beta=1/(tf+273) Ral=g*beta*(Ts-T)*Lc^3*Pr/kv^2 Nu=0.54*Ral^(1/4) h=Nu*k/Lc Q=h*As*(Ts-T) %Heat Sink-------------------------------------------- S=0.52e-2; % We can change it H=1.3e-2; % We can change it (2.54e-2