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il63 [147K]
3 years ago
14

A plane wall, 7.5 cm thick, generates heat internally at the rate of 105W/m3. One side of the wall is insulated and the other si

de is exposed to fluid with T[infinity]= 90 °C and h= 500 W/m2-K. If the thermal conductivity of the wall is 12 W/(m K), calculate the temperature in the center of the wall.
Engineering
1 answer:
lukranit [14]3 years ago
4 0

Answer:

T=128°C

Explanation:

Given Data:

thickness = 7.5 cm ;

internal heat generation rate = q_{s} = 105W/m³ ;

First we have the equation of conduction for steady state withh heat generation as:

k\frac{d^{2}T }{dx^{2} } + q_{s} = 0

by re-arranging it we get

\frac{d^{2}T }{dx^{2} } = - q_{s}/k

Here, q_{s} is the rate of internal heat generation,

          k is thermal conductivity constant

          dT is temperature differential

          dx is differential along x-axis

Now if we integrate both sides w.r.t x, one derivative is removed from left side of equation and and a variable is multiplied to the term on the right side and a unknown integrating constant C is added.

\frac{dT}{dx}= - (q_{s}/k)*x + C -------------------- equation (1)

Now if we apply Dirichlet's first boundary equation at x = 0, dT/dx = 0

we get,

\frac{dT}{dx}= - (q_{s}/k)*x + C

0 = - (q_{s}/k)*0 + C

C = 0

Now put C = 0 in equation 1

we get,

k \frac{dT}{dx}= - q_{s}*x ------------------ equation (2)

Now integrate it w.r.t x

T= - (q_{s}/2k)*x² + C₁ ------------------ equation (3)

Now apply Dirichlet's second boundary condition on equation 2, i.e, x=L,       k\frac{dT}{dx} = h⁻(T-T₀), equation 2 becomes

h⁻(T-T₀) = Lq_{s} ------------------ equation (4)

Put value of T from equation 3 in equation 4

h⁻(- (q_{s}/2k)*L² + C₁-T₀) = Lq_{s}

By rearranging it we get,

C₁= T₀ + q_{s}L[(L/2k)+(1/h⁻)]  ------------------ equation (5)

Now putting value of C₁ from equation 5 in equation 3, we get

T = T₀ + (q_{s}/2k)[L² + 2kL/h⁻]

Now by putting the given values of  T₀ = 90°C, q_{s} = 10 W/m², k = 12 W/mK, L = 0.075m, h⁻ = 500 W/m²K

we get, T= 128°C

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We now need to know the yield stress or the ultimate stress for each material. We use the AISI and ASTM charts for steels, materials charts for non-ferrous materials and plastics safety charts for the plastic materials.

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DF=\displaystyle\frac{34.72MPa}{385MPa}=0.09

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DF=\displaystyle\frac{34.72MPa}{275.8MPa}=0.125

D) The yield stress of aluminum allot 6061-T6 is 290 MPa, therefore:

DF=\displaystyle\frac{34.72MPa}{290MPa}=0.12

E) The yield stress of titanium alloy Ti-6Al-4V annealed (certified by manufacturers) is 880 MPa, therefore:

DF=\displaystyle\frac{34.72MPa}{880MPa}=0.039

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