A rectangular lamina of width a and height b is sandwiched between two slabs of ice, so that the lower and upper sides, of width a, are at a temperature Θ 0, The other two sides are thermally isolat...
The upper and lower sides of the rectangular aluminum block L-10mm, D 3mm) are insulated as shown below. The left and right sides have temperature boundary conditions and convective boundary conditions, respectively Surface temperature T 100 C, Outside temperature T-20 C Heat transfer coefficent h 120W/(m2 k) Alumium thermal conductivity K-220 W/(m k), density p-2707kg/m Specific heat C896J/(kg K) Assuming the aluminum block is a two-dimensional shape, calculate the temperature on the plane(x-y) as follows. 1) Calculate the temperature of...
You will need to use program like Matlab.
The upper and lower sides of the rectangular aluminum block(L-10mm, D-3mm) are insulated as shown below. The left and right sides have temperature boundary conditions and convective boundary conditions, respectively. Surface temperature T 100 C, Outside te Heat transfer coefficent h 120W/(m2k) mperatureT -20 C Alumium thermal conductivity K-220 W ( Specific heat C-896J/ (kg K) k), density p 2707kg/m3, Assuming the aluminum block is a two-dimensional shape, calculate the temperature on...
3. (20 points) Denote u(ar, y) the steady-state temperature in a rectangle area 0 z 10, 0yS 1. Find the temperature in the rectangle if the temperature on the up side is kept at 0°, the lower side at 10° while the temperature on the left side is S0)= sin(y) and the right side is insulated. Answer the following questions. (a) (10 points) Write the Dirichlet problem including the Laplace's equation in two dimensions and the boundary conditions. (b) (10...
And governing equation used
Written A rectangular plane wing can be treated as a two-dimensional domain as a rough approximation. The length of the wing is 3 and its width (the height of the domain when represented on a sheet of paper) is 1. The wing is exposed to a heat source at its leftmost edge, with a temperature equal to Trot. The flux of heat in the wing is given by Fourier's law: and throughout the domain a source...