The cross section of a long circular tube, which is divided mw two semicylindrical ducts by a thin wall, is shown. Sides 1 and 2 are maintained at temperatures of T 1 = 600 K and T 2 = 400 K , respectively, while the mean temperatures of gas flows through ducts 1 and 2 are T g , 1 = 571 K and T g , 2 = 449 K , respectively. The foregoing temperatures are invariant in the axial direction. The gases provide surface convection coefficients of h 1 = h 2 = 5 W/m 2 ⋅ K while all duct surfaces may be approximated as blackbodies ( ε 1 = ε 2 = ε w = 1 ) . What is the duct wall temperature, T w ? By performing an energy balance on the gas in side 1, verify that T g , 1 is, in fact equal to 571 K.
The cross section of a long circular tube, which is divided mw two semicylindrical ducts by a thin wall, is shown. Sides 1 and 2 are maintained at temperatures of T 1 = 600 K and T 2 = 400 K , respectively, while the mean temperatures of gas flows through ducts 1 and 2 are T g , 1 = 571 K and T g , 2 = 449 K , respectively. The foregoing temperatures are invariant in the axial direction. The gases provide surface convection coefficients of h 1 = h 2 = 5 W/m 2 ⋅ K while all duct surfaces may be approximated as blackbodies ( ε 1 = ε 2 = ε w = 1 ) . What is the duct wall temperature, T w ? By performing an energy balance on the gas in side 1, verify that T g , 1 is, in fact equal to 571 K.
Solution Summary: The author explains the energy balance equation for the duct wall temperature and the surface convection of coefficients.
The cross section of a long circular tube, which is divided mw two semicylindrical ducts by a thin wall, is shown.
Sides 1 and 2 are maintained at temperatures of
T
1
=
600
K
and
T
2
=
400
K
, respectively, while the mean temperatures of gas flows through ducts 1 and 2 are
T
g
,
1
=
571
K
and
T
g
,
2
=
449
K
, respectively. The foregoing temperatures are invariant in the axial direction. The gases provide surface convection coefficients of
h
1
=
h
2
=
5
W/m
2
⋅
K
while all duct surfaces may be approximated as blackbodies
(
ε
1
=
ε
2
=
ε
w
=
1
)
. What is the duct wall temperature, Tw? By performing an energy balance on the gas in side 1, verify that Tg,1 is, in fact equal to 571 K.
The beam is made of elastic perfectly plastic material. Determine the shape factor for the cross
section of the beam (Figure Q3). [Take σy = 250 MPa, yNA = 110.94 mm, I = 78.08 x 106 mm²]
y
25 mm
75 mm
I
25 mm
200 mm
25 mm
125
Figure Q3
A beam of the cross section shown in Figure Q3 is made of a steel that is assumed to be elastic-
perfectectly plastic material with E = 200 GPa and σy = 240 MPa. Determine:
i.
The shape factor of the cross section
ii.
The bending moment at which the plastic zones at the top and bottom of the bar are 30
mm thick.
15 mm
30 mm
15 mm
30 mm
30 mm
30 mm
A torque of magnitude T = 12 kNm is applied to the end of a tank containing compressed air
under a pressure of 8 MPa (Figure Q1). The tank has a 180 mm inner diameter and a 12 mm
wall thickness. As a result of several tensile tests, it has been found that tensile yeild strength
is σy = 250 MPa for thr grade of steel used. Determine the factor of safety with respect to yeild,
using:
(a) The maximum shearing stress theory
(b) The maximum distortion energy theory
T
Figure Q1
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