Consider the diffuse, gray opaque disk A 1 , which has a diameter of 10 mm, an emissivity of 0.3, and is at a temperature of 400 K. Coaxial to the disk A 1 , there is a black, ring-shaped disk A 2 at 1000K having the dimensions shown in the sketch. The backside of A 2 is insulated and does not directly irradiate the cryogenically cooled detector disk A 3 , which is of diameter 10 mm and is located 2 m from A 1 Calculate the rate at which radiation is incident on A 3 due to emission and reflection from A 1 .
Consider the diffuse, gray opaque disk A 1 , which has a diameter of 10 mm, an emissivity of 0.3, and is at a temperature of 400 K. Coaxial to the disk A 1 , there is a black, ring-shaped disk A 2 at 1000K having the dimensions shown in the sketch. The backside of A 2 is insulated and does not directly irradiate the cryogenically cooled detector disk A 3 , which is of diameter 10 mm and is located 2 m from A 1 Calculate the rate at which radiation is incident on A 3 due to emission and reflection from A 1 .
Solution Summary: The author explains the rate at which radiation is incident on A_3 due to emission and reflection.
Consider the diffuse, gray opaque disk
A
1
, which has a diameter of 10 mm, an emissivity of 0.3, and is at a temperature of 400 K. Coaxial to the disk
A
1
, there is a black, ring-shaped disk
A
2
at 1000K having the dimensions shown in the sketch. The backside of
A
2
is insulated and does not directly irradiate the cryogenically cooled detector disk
A
3
, which is of diameter 10 mm and is located 2 m from
A
1
Calculate the rate at which radiation is incident on
A
3
due to emission and reflection from
A
1
.
An engineered passive radiative cooler coating is placed under the Sun. Provided the following simplified spectral emissivity/absorptivity plot below, calculate the total diffuse emissivity and absorptivity if its uniform surface temperature is a Ts=20°C. Assume the Sun's irradiation onk Earth is Gsun=1380 W/m2 and its blackbody temperature is Tsun= 5800K. Ignore the radiation from the atmosphere (surroundings).
Two large parallel surfaces (surface 1 and surface 2) kept at constant surface temperature of T1= 300 °C
and T2= 100 °C. The two surfaces have emissivity of ɛ1= 0.8 and ɛ2= 0.5 respectively. The top surface
(surface 2) is cooled by convective heat transfer with surrounding air temperature of 20 °C. The bottom
surface (surface 1) is well insulated at the backside. Assume the surfaces are diffuse and gray, and the
space between the surfaces is vacuum.
a. Calculate the radiation heat transfer between the surfaces per unit area [W/m?].
b. Calculate the convective heat transfer coefficient for the top surface [W/m2 K].
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