A square isothermal chip is of width w = 5 mm on aside and is mounted in a substrate such that its side andback surfaces are well insulated; the front surface isexposed to the how of a coolant at T ∞ = 15 ° C . Frontreliability considerations, the chip temperature must notexceed T = 85 ° C . If the coolant is air and the corresponding convectioncoefficient is h = 200 W/m 2 ⋅ K , what is the maximumallowable chip power? If the coolant is a dielectricliquid for which h = 300 W/m 2 ⋅ K , what is the maximum allowable power?
A square isothermal chip is of width w = 5 mm on aside and is mounted in a substrate such that its side andback surfaces are well insulated; the front surface isexposed to the how of a coolant at T ∞ = 15 ° C . Frontreliability considerations, the chip temperature must notexceed T = 85 ° C . If the coolant is air and the corresponding convectioncoefficient is h = 200 W/m 2 ⋅ K , what is the maximumallowable chip power? If the coolant is a dielectricliquid for which h = 300 W/m 2 ⋅ K , what is the maximum allowable power?
Solution Summary: The author explains the maximum allowable chip power with air and with dielectric liquid as coolant.
A square isothermal chip is of width
w
=
5
mm
on aside and is mounted in a substrate such that its side andback surfaces are well insulated; the front surface isexposed to the how of a coolant at
T
∞
=
15
°
C
. Frontreliability considerations, the chip temperature must notexceed
T
=
85
°
C
.
If the coolant is air and the corresponding convectioncoefficient is
h
=
200
W/m
2
⋅
K
, what is the maximumallowable chip power? If the coolant is a dielectricliquid for which
h
=
300
W/m
2
⋅
K
, what is the maximum allowable power?
cylindrical fuel element for a gas-cooled nuclear reactor, the heat generation rate within the fuel element due to fission can be approximated by the relation: q(r) = q_0 [1 - (r/a)^2] W/m^3 where a is the radius of the fuel element and q_0 is constant. The boundary surface at r = a is maintained at a uniform temperature T_0. Assuming one-dimensional, steady-state heat flow, develop a relation for the temperature drop from the centerline to the surface of the fuel element. For radius a= 30mm, the thermal conductivity k = 10 W/m middot K and q_0 = 2 times 10^7 W/m^3, calculate the temperature drop from the centerline to the surface.
A thick-walled cylindrical tubing of hard rubber (k=0.151 W/m*K) having an inside radius of 5 mm and an outside radius of 20 mm is being used as a temporary cooling coil in a bath. Ice water is flowing rapidly inside, and the inside wall temperature is 275 K. The outside surface temperature is 300 K. A total of 20 W must be removed from the bath by the cooling coil. How many meter of tubing are needed?
Engine Oil at 58.95 degrees celsius Flows over a 5m long flat plate whose temperature is 20.11 degrees celsius with a velocity of 2.2m/s. Determine the rate of heat transfer (W), considering forced convection, per unit width of the entire plate.
Density = 876kg/m^3
Thermal conductivity = 0.144W/m-K
Pr = 2870
dynamic viscosity = 0.21kg/m-s
Q = ?
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