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
.
Both portions of the rod ABC are made of an aluminum for which E = 70 GPa.
Based on the given information find:
1- deformation at A
2- stress in BC
3- Total strain
4- If v (Poisson ratio is 0.25, find the
lateral deformation of AB
Last 3 student ID+ 300 mm=L2
724
A
P=Last 2 student ID+ 300 KN
24
24
Diameter Last 2 student ID+ 15 mm
Last 3 student ID+ 500 mm=L1
724
C
B
24
Q=Last 2 student ID+ 100 KN
24
Diameter Last 2 student ID+ 40 mm
Q2Two wooden members of uniform cross section are joined by the simple scarf splice shown. Knowing that the
maximum allowable tensile stress in the glued splice is 75 psi, determine (a) the largest load P that can be safely
supported, (b) the corresponding shearing stress in the splice.
น
Last 1 student ID+5 inch=W
=9
4
L=Last 1 student ID+8 inch
=12
60°
P'
Q4
The two solid shafts are connected by gears as shown and are made of a steel for which the allowable shearing
stress is 7000 psi. Knowing the diameters of the two shafts are, respectively, dBC
determine the largest torque Tc that can be applied at C.
4
and dEF
dBC=Last 1 student ID+3 inch
dEF=Last 1 student ID+1 inch
7
R=Last 1 Student ID+5 inch
9
R
B
Tc
2.5 in.
E
TF
H
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