A homeowner's wood stove is equipped with a top burner for cooking. The D = 200 -mm -diameter burner is fabricated of east iron ( k = 65 W/m ⋅ K ) . The bottom (combustion) side of the burner has 8 straight fins of uniform cross section, arranged as shown in the sketch. A very thin ceramic coating ( ε = 0.95 ) is applied to all surfaces of the burner. The top of the burner is exposed to room conditions ( T sur,t = T ∞ , t = 20 ° C, h t = 40 W/m 2 ⋅ K ) , while the bottom of the burner is exposed to combustion conditions ( T sur , b = T ∞ , b = 450 ° C , h b = 50 W/m 2 ⋅ K ) . Compare the top surface temperature of the finned burner to that which would exist for a burner without fins. Hint: Use the same expression for radiation heat transfer to the bottom of the tinned burner as for the burner with no fins.
A homeowner's wood stove is equipped with a top burner for cooking. The D = 200 -mm -diameter burner is fabricated of east iron ( k = 65 W/m ⋅ K ) . The bottom (combustion) side of the burner has 8 straight fins of uniform cross section, arranged as shown in the sketch. A very thin ceramic coating ( ε = 0.95 ) is applied to all surfaces of the burner. The top of the burner is exposed to room conditions ( T sur,t = T ∞ , t = 20 ° C, h t = 40 W/m 2 ⋅ K ) , while the bottom of the burner is exposed to combustion conditions ( T sur , b = T ∞ , b = 450 ° C , h b = 50 W/m 2 ⋅ K ) . Compare the top surface temperature of the finned burner to that which would exist for a burner without fins. Hint: Use the same expression for radiation heat transfer to the bottom of the tinned burner as for the burner with no fins.
A homeowner's wood stove is equipped with a top burner for cooking. The
D
=
200
-mm
-diameter burner is fabricated of east iron
(
k
=
65
W/m
⋅
K
)
.
The bottom (combustion) side of the burner has 8 straight fins of uniform cross section, arranged as shown in the sketch. A very thin ceramic coating
(
ε
=
0.95
)
is applied to all surfaces of the burner. The top of the burner is exposed to room conditions
(
T
sur,t
=
T
∞
,
t
=
20
°
C,
h
t
=
40
W/m
2
⋅
K
)
,
while the bottom of the burner is exposed to combustion conditions
(
T
sur
,
b
=
T
∞
,
b
=
450
°
C
,
h
b
=
50
W/m
2
⋅
K
)
.
Compare the top surface temperature of the finned burner to that which would exist for a burner without fins. Hint: Use the same expression for radiation heat transfer to the bottom of the tinned burner as for the burner with no fins.
Assume a Space Launch System (Figure 1(a)) that is approximated as a cantilever undamped single degree of freedom (SDOF) system with a mass at its free end (Figure 1(b)). The cantilever is assumed to be massless. Assume a wind load that is approximated with a concentrated harmonic forcing function p(t) = posin(ωt) acting on the mass. The known properties of the SDOF and the applied forcing function are given below. • Mass of SDOF: m =120 kip/g • Acceleration of gravity: g = 386 in/sec2 • Bending sectional stiffness of SDOF: EI = 1015 lbf×in2 • Height of SDOF: h = 2000 inches • Amplitude of forcing function: po = 6 kip • Forcing frequency: f = 8 Hz Figure 1: Single-degree-of-freedom system in Problem 1. Please compute the following considering the steady-state response of the SDOF system. Do not consider the transient response unless it is explicitly stated in the question. (a) The natural circular frequency and the natural period of the SDOF. (10 points) (b) The maximum displacement of…
Assume a Space Launch System (Figure 1(a)) that is approximated as a cantilever undamped single degree of freedom (SDOF) system with a mass at its free end (Figure 1(b)). The cantilever is assumed to be massless. Assume a wind load that is approximated with a concentrated harmonic forcing function p(t) = posin(ωt) acting on the mass. The known properties of the SDOF and the applied forcing function are given below. • Mass of SDOF: m =120 kip/g • Acceleration of gravity: g = 386 in/sec2 • Bending sectional stiffness of SDOF: EI = 1015 lbf×in2 • Height of SDOF: h = 2000 inches • Amplitude of forcing function: po = 6 kip • Forcing frequency: f = 8 Hz Figure 1: Single-degree-of-freedom system in Problem 1. Please compute the following considering the steady-state response of the SDOF system. Do not consider the transient response unless it is explicitly stated in the question. (a) The natural circular frequency and the natural period of the SDOF. (10 points) (b) The maximum displacement of…
Please solve
13 * √(2675.16)² + (63.72 + 2255,03)² = 175x106
can you explain the process for
getting d seperate thank you
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