The oxidized-aluminum wing of an aircraft has a chord length of Lc ◰ 4 m and a spectral, hemispher- ical emissivity characterized by the following distribution. (a)Consider conditions for which the plane is on the ground where the air temperature is 27 ∘ C , the solar irradiation is 800 W/m 2 , and the effective sky temperature is 270 K. If the air is quiescent, what is the temperature of the top surface of the wing? The wing may be approximated as a horizontal, flat plate. (b) When the aircraft is flying at an elevation of approximately 9000 m and a speed of 200 m/s, the air temperature, solar irradiation, and effective sky temperatureare − 40 ∘ C , 1100 W/m 2 and 235K , respectively. What is the temperature of the wing’s top surface? The properties of the air may be approximated as ρ = 0.470 kg/m 3 , μ =1 .50x10 − 5 N ⋅ s / m 2 , K = 0.021 W/m ⋅ K, and Pr =0 .72 .
The oxidized-aluminum wing of an aircraft has a chord length of Lc ◰ 4 m and a spectral, hemispher- ical emissivity characterized by the following distribution. (a)Consider conditions for which the plane is on the ground where the air temperature is 27 ∘ C , the solar irradiation is 800 W/m 2 , and the effective sky temperature is 270 K. If the air is quiescent, what is the temperature of the top surface of the wing? The wing may be approximated as a horizontal, flat plate. (b) When the aircraft is flying at an elevation of approximately 9000 m and a speed of 200 m/s, the air temperature, solar irradiation, and effective sky temperatureare − 40 ∘ C , 1100 W/m 2 and 235K , respectively. What is the temperature of the wing’s top surface? The properties of the air may be approximated as ρ = 0.470 kg/m 3 , μ =1 .50x10 − 5 N ⋅ s / m 2 , K = 0.021 W/m ⋅ K, and Pr =0 .72 .
Solution Summary: The author explains the formula used to calculate the surface temperature of the wing: solar irradiation, air temperature, emissivity, and heat transfer coefficient.
The oxidized-aluminum wing of an aircraft has a chord length of Lc ◰ 4 m and a spectral, hemispher- ical emissivity characterized by the following distribution.
(a)Consider conditions for which the plane is on the ground where the air temperature is
27
∘
C
, the solar irradiation is
800 W/m
2
, and the effective sky temperature is 270 K. If the air is quiescent, what is the temperature of the top surface of the wing? The wing may be approximated as a horizontal, flat plate.
(b) When the aircraft is flying at an elevation of approximately 9000 m and a speed of 200 m/s, the air temperature, solar irradiation, and effective sky temperatureare
−
40
∘
C
,
1100
W/m
2
and 235K
, respectively. What is the temperature of the wing’s top surface? The properties of the air may be approximated as
ρ
=
0.470
kg/m
3
,
μ
=1
.50x10
−
5
N
⋅
s
/
m
2
,
K
=
0.021
W/m
⋅
K, and Pr =0
.72
.
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.