Answer:
1. ![\dot Q=19600\ W](https://tex.z-dn.net/?f=%5Cdot%20Q%3D19600%5C%20W)
2. ![\dot Q=120\ W](https://tex.z-dn.net/?f=%5Cdot%20Q%3D120%5C%20W)
Explanation:
1.
Given:
- height of the window pane,
![h=2\ m](https://tex.z-dn.net/?f=h%3D2%5C%20m)
- width of the window pane,
![w=1\ m](https://tex.z-dn.net/?f=w%3D1%5C%20m)
- thickness of the pane,
![t=5\ mm= 0.005\ m](https://tex.z-dn.net/?f=t%3D5%5C%20mm%3D%200.005%5C%20m)
- thermal conductivity of the glass pane,
![k_g=1.4\ W.m^{-1}.K^{-1}](https://tex.z-dn.net/?f=k_g%3D1.4%5C%20W.m%5E%7B-1%7D.K%5E%7B-1%7D)
- temperature of the inner surface,
![T_i=15^{\circ}C](https://tex.z-dn.net/?f=T_i%3D15%5E%7B%5Ccirc%7DC)
- temperature of the outer surface,
![T_o=-20^{\circ}C](https://tex.z-dn.net/?f=T_o%3D-20%5E%7B%5Ccirc%7DC)
<u>According to the Fourier's law the rate of heat transfer is given as:</u>
![\dot Q=k_g.A.\frac{dT}{dx}](https://tex.z-dn.net/?f=%5Cdot%20Q%3Dk_g.A.%5Cfrac%7BdT%7D%7Bdx%7D)
here:
A = area through which the heat transfer occurs = ![2\times 1=2\ m^2](https://tex.z-dn.net/?f=2%5Ctimes%201%3D2%5C%20m%5E2)
dT = temperature difference across the thickness of the surface = ![35^{\circ}C](https://tex.z-dn.net/?f=35%5E%7B%5Ccirc%7DC)
dx = t = thickness normal to the surface = ![0.005\ m](https://tex.z-dn.net/?f=0.005%5C%20m)
![\dot Q=1.4\times 2\times \frac{35}{0.005}](https://tex.z-dn.net/?f=%5Cdot%20Q%3D1.4%5Ctimes%202%5Ctimes%20%5Cfrac%7B35%7D%7B0.005%7D)
![\dot Q=19600\ W](https://tex.z-dn.net/?f=%5Cdot%20Q%3D19600%5C%20W)
2.
- air spacing between two glass panes,
![dx=0.01\ m](https://tex.z-dn.net/?f=dx%3D0.01%5C%20m)
- area of each glass pane,
![A=2\times 1=2\ m^2](https://tex.z-dn.net/?f=A%3D2%5Ctimes%201%3D2%5C%20m%5E2)
- thermal conductivity of air,
![k_a=0.024\ W.m^{-1}.K^{-1}](https://tex.z-dn.net/?f=k_a%3D0.024%5C%20W.m%5E%7B-1%7D.K%5E%7B-1%7D)
- temperature difference between the surfaces,
![dT=25^{\circ}C](https://tex.z-dn.net/?f=dT%3D25%5E%7B%5Ccirc%7DC)
<u>Assuming layered transfer of heat through the air and the air between the glasses is always still:</u>
![\dot Q=k_a.A.\frac{dT}{dx}](https://tex.z-dn.net/?f=%5Cdot%20Q%3Dk_a.A.%5Cfrac%7BdT%7D%7Bdx%7D)
![\dot Q=0.024\times 2\times \frac{25}{0.01}](https://tex.z-dn.net/?f=%5Cdot%20Q%3D0.024%5Ctimes%202%5Ctimes%20%5Cfrac%7B25%7D%7B0.01%7D)
![\dot Q=120\ W](https://tex.z-dn.net/?f=%5Cdot%20Q%3D120%5C%20W)
Answer:
![Hr=4.2*10^7\ btu/hr](https://tex.z-dn.net/?f=Hr%3D4.2%2A10%5E7%5C%20btu%2Fhr)
Explanation:
From the question we are told that:
Water flow Rate ![R=4.5slug/s=144.78ib/sec](https://tex.z-dn.net/?f=R%3D4.5slug%2Fs%3D144.78ib%2Fsec)
Initial Temperature ![T_1=60 \textdegree F](https://tex.z-dn.net/?f=T_1%3D60%20%5Ctextdegree%20F)
Final Temperature ![T_2=140 \textdegree F](https://tex.z-dn.net/?f=T_2%3D140%20%5Ctextdegree%20F)
Let
Specific heat of water ![\gamma= 1](https://tex.z-dn.net/?f=%5Cgamma%3D%201)
And
![\triangle T= 140-60](https://tex.z-dn.net/?f=%5Ctriangle%20T%3D%20140-60)
![\triangle T= 80\ Deg.F](https://tex.z-dn.net/?f=%5Ctriangle%20T%3D%2080%5C%20Deg.F)
Generally the equation for Heat transfer rate of water
is mathematically given by
Heat transfer rate to water= mass flow rate* specific heat* change in temperature
![H_r=R* \gamma*\triangle T](https://tex.z-dn.net/?f=H_r%3DR%2A%20%5Cgamma%2A%5Ctriangle%20T)
![H_r=144.78*80*1](https://tex.z-dn.net/?f=H_r%3D144.78%2A80%2A1)
![H_r=11582.4\ btu/sec](https://tex.z-dn.net/?f=H_r%3D11582.4%5C%20btu%2Fsec)
Therefore
![H_r=11582.4\ btu/sec*3600](https://tex.z-dn.net/?f=H_r%3D11582.4%5C%20btu%2Fsec%2A3600)
![Hr=4.2*10^7\ btu/hr](https://tex.z-dn.net/?f=Hr%3D4.2%2A10%5E7%5C%20%20btu%2Fhr)
Answer: 8.33333333 or 6.1989778
Explanation:
Answer:
0.024 m = 24.07 mm
Explanation:
1) Notation
= tensile stress = 200 Mpa
= plane strain fracture toughness= 55 Mpa![\sqrt{m}](https://tex.z-dn.net/?f=%5Csqrt%7Bm%7D)
= length of a surface crack (Variable of interest)
2) Definition and Formulas
The Tensile strength is the ability of a material to withstand a pulling force. It is customarily measured in units (F/A), like the pressure. Is an important concept in engineering, especially in the fields of materials and structural engineering.
By definition we have the following formula for the tensile stress:
(1)
We are interested on the minimum length of a surface that will lead to a fracture, so we need to solve for ![\lambda](https://tex.z-dn.net/?f=%5Clambda)
Multiplying both sides of equation (1) by ![Y\sqrt{\pi\lambda}](https://tex.z-dn.net/?f=Y%5Csqrt%7B%5Cpi%5Clambda%7D)
(2)
Sequaring both sides of equation (2):
(3)
Dividing both sides by
we got:
(4)
Replacing the values into equation (4) we got:
![\lambda=\frac{1}{\pi}[\frac{55 Mpa\sqrt{m}}{1.0(200Mpa)}]^2 =0.02407m](https://tex.z-dn.net/?f=%5Clambda%3D%5Cfrac%7B1%7D%7B%5Cpi%7D%5B%5Cfrac%7B55%20Mpa%5Csqrt%7Bm%7D%7D%7B1.0%28200Mpa%29%7D%5D%5E2%20%3D0.02407m)
3) Final solution
So the minimum length of a surface crack that will lead to fracture, would be 24.07 mm or more.