Answer:
a) The local drag at the midpoint is 0.921 N/m²
b) The drag force is 0.059 N
c) The local heat transfer is 27158.6 W/m²
d) The total heat transfer is 17282.5 W
Explanation:
Given:
ρ = 13557.5 kg/m³
v = 0.1165x10⁻⁶m²/s
Pr = 0.026
k = 8.5675 W/m K
vα = 0.3 m/s
Tα = 15°C
a) The Reynold´s number is:
![Re=\frac{0.3*0.15}{0.1165x10^{-6} } =3.863x10^{5} ,Re](https://tex.z-dn.net/?f=Re%3D%5Cfrac%7B0.3%2A0.15%7D%7B0.1165x10%5E%7B-6%7D%20%7D%20%3D3.863x10%5E%7B5%7D%20%2CRe%3C5x10%5E%7B5%7D)
The flow is laminar. The drag coefficient at the midpoint is:
![C_{fn} =\frac{0.664}{\sqrt{Ren} } =\frac{0.664}{\sqrt{\frac{v_{\alpha } *0.075}{v} } } =\frac{0.664}{\sqrt{\frac{0.3*0.075}{0.1165x10^{-6} } } } =0.00151](https://tex.z-dn.net/?f=C_%7Bfn%7D%20%3D%5Cfrac%7B0.664%7D%7B%5Csqrt%7BRen%7D%20%7D%20%3D%5Cfrac%7B0.664%7D%7B%5Csqrt%7B%5Cfrac%7Bv_%7B%5Calpha%20%7D%20%2A0.075%7D%7Bv%7D%20%7D%20%7D%20%3D%5Cfrac%7B0.664%7D%7B%5Csqrt%7B%5Cfrac%7B0.3%2A0.075%7D%7B0.1165x10%5E%7B-6%7D%20%7D%20%7D%20%7D%20%3D0.00151)
The local drag at the midpoint is equal:
![\tau =\frac{C_{fn}PV_{\alpha }^{2} }{2} =\frac{0.0015*13557.5*0.3^{2} }{2} =0.921N/m^{2}](https://tex.z-dn.net/?f=%5Ctau%20%3D%5Cfrac%7BC_%7Bfn%7DPV_%7B%5Calpha%20%7D%5E%7B2%7D%20%20%20%7D%7B2%7D%20%3D%5Cfrac%7B0.0015%2A13557.5%2A0.3%5E%7B2%7D%20%7D%7B2%7D%20%3D0.921N%2Fm%5E%7B2%7D)
b) The average coefficient for the plate is:
![C_{D} =2*\frac{0.664}{\sqrt{ReL} } =2*\frac{0.664}{\sqrt{\frac{0.3*0.15}{0.1165x10^{-6} } } } =0.00214](https://tex.z-dn.net/?f=C_%7BD%7D%20%3D2%2A%5Cfrac%7B0.664%7D%7B%5Csqrt%7BReL%7D%20%7D%20%3D2%2A%5Cfrac%7B0.664%7D%7B%5Csqrt%7B%5Cfrac%7B0.3%2A0.15%7D%7B0.1165x10%5E%7B-6%7D%20%7D%20%7D%20%7D%20%3D0.00214)
The total drag force is:
![F_{D} =\frac{C_{D}Pv_{\alpha }^{2}A }{2} =\frac{0.0024*13557.5*0.3^{2}*0.15*0.3 }{2} =0.059N](https://tex.z-dn.net/?f=F_%7BD%7D%20%3D%5Cfrac%7BC_%7BD%7DPv_%7B%5Calpha%20%7D%5E%7B2%7DA%20%20%20%7D%7B2%7D%20%3D%5Cfrac%7B0.0024%2A13557.5%2A0.3%5E%7B2%7D%2A0.15%2A0.3%20%7D%7B2%7D%20%3D0.059N)
c) The equation:
![Nv_{n} =\frac{h-n}{k} =0.332Re^{1/2} Pr^{1/3}](https://tex.z-dn.net/?f=Nv_%7Bn%7D%20%3D%5Cfrac%7Bh-n%7D%7Bk%7D%20%3D0.332Re%5E%7B1%2F2%7D%20Pr%5E%7B1%2F3%7D)
at midpoint n = 0.075 m
![\frac{h-0.075}{8.5675} =0.332\sqrt{\frac{0.3*0.075}{0.1165x10^{-6} } } *(0.026)^{1/3} \\h=4937.6W/m^{2} K](https://tex.z-dn.net/?f=%5Cfrac%7Bh-0.075%7D%7B8.5675%7D%20%3D0.332%5Csqrt%7B%5Cfrac%7B0.3%2A0.075%7D%7B0.1165x10%5E%7B-6%7D%20%7D%20%7D%20%2A%280.026%29%5E%7B1%2F3%7D%20%5C%5Ch%3D4937.6W%2Fm%5E%7B2%7D%20K)
The local heat transfer is:
![Q=h(T_{plate} -T_{\alpha } )=4937.6(70-15)=27158.6W/m^{2}](https://tex.z-dn.net/?f=Q%3Dh%28T_%7Bplate%7D%20-T_%7B%5Calpha%20%7D%20%29%3D4937.6%2870-15%29%3D27158.6W%2Fm%5E%7B2%7D)
d) The average heat coefficient is:
![h_{v} =2hL=0.15\\](https://tex.z-dn.net/?f=h_%7Bv%7D%20%3D2hL%3D0.15%5C%5C)
The average Nussele:
![\frac{h*0.5}{8.5675} =0.644(\frac{0.3*0.15}{0.1165x10^{-6} } )^{1/2} *(0.016)^{1/3} \\h=6982.8W/m^{2} K](https://tex.z-dn.net/?f=%5Cfrac%7Bh%2A0.5%7D%7B8.5675%7D%20%3D0.644%28%5Cfrac%7B0.3%2A0.15%7D%7B0.1165x10%5E%7B-6%7D%20%7D%20%29%5E%7B1%2F2%7D%20%2A%280.016%29%5E%7B1%2F3%7D%20%5C%5Ch%3D6982.8W%2Fm%5E%7B2%7D%20K)
![Q_{T} =Ah(T_{plate} -T_{\alpha } )=0.15*0.3*3982.8*(70-5)=17282.5W](https://tex.z-dn.net/?f=Q_%7BT%7D%20%3DAh%28T_%7Bplate%7D%20-T_%7B%5Calpha%20%7D%20%29%3D0.15%2A0.3%2A3982.8%2A%2870-5%29%3D17282.5W)