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
Step-by-step 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=(0.3*0.15)/(0.1165x10^(-6) ) =3.863x10^(5) ,Re<5x10^(5)](https://img.qammunity.org/2021/formulas/physics/college/c1fp3tz8tj0vm2w1id7f1inkvz18d8d30g.png)
The flow is laminar. The drag coefficient at the midpoint is:
![C_(fn) =(0.664)/(√(Ren) ) =\frac{0.664}{\sqrt{(v_(\alpha ) *0.075)/(v) } } =\frac{0.664}{\sqrt{(0.3*0.075)/(0.1165x10^(-6) ) } } =0.00151](https://img.qammunity.org/2021/formulas/physics/college/7kpfhspouaoupf59x40479qn2o1vymxi6f.png)
The local drag at the midpoint is equal:
![\tau =(C_(fn)PV_(\alpha )^(2) )/(2) =(0.0015*13557.5*0.3^(2) )/(2) =0.921N/m^(2)](https://img.qammunity.org/2021/formulas/physics/college/drz0aq1lkd4x4vl2hcjnwi1iakprsnpowd.png)
b) The average coefficient for the plate is:
![C_(D) =2*(0.664)/(√(ReL) ) =2*\frac{0.664}{\sqrt{(0.3*0.15)/(0.1165x10^(-6) ) } } =0.00214](https://img.qammunity.org/2021/formulas/physics/college/b3fauf8rp43v9z5ulf92fei82z773tvcvh.png)
The total drag force is:
![F_(D) =(C_(D)Pv_(\alpha )^(2)A )/(2) =(0.0024*13557.5*0.3^(2)*0.15*0.3 )/(2) =0.059N](https://img.qammunity.org/2021/formulas/physics/college/e0p1t70vnorsdqr2y23p9qf7h4ckibknzu.png)
c) The equation:
![Nv_(n) =(h-n)/(k) =0.332Re^(1/2) Pr^(1/3)](https://img.qammunity.org/2021/formulas/physics/college/aaptklehwg2m2uvk2d43hny9dprfzoefnr.png)
at midpoint n = 0.075 m
![(h-0.075)/(8.5675) =0.332\sqrt{(0.3*0.075)/(0.1165x10^(-6) ) } *(0.026)^(1/3) \\h=4937.6W/m^(2) K](https://img.qammunity.org/2021/formulas/physics/college/fvg1t674pn154xsz37v2u7x9ba9iaq6mtj.png)
The local heat transfer is:
![Q=h(T_(plate) -T_(\alpha ) )=4937.6(70-15)=27158.6W/m^(2)](https://img.qammunity.org/2021/formulas/physics/college/v7cg11mgu1bp4t01afb8h7h5z1rqgpt4xo.png)
d) The average heat coefficient is:
![h_(v) =2hL=0.15\\](https://img.qammunity.org/2021/formulas/physics/college/gslmq90kmq3rzllakhgudkivfmlfkqmdig.png)
The average Nussele:
![(h*0.5)/(8.5675) =0.644((0.3*0.15)/(0.1165x10^(-6) ) )^(1/2) *(0.016)^(1/3) \\h=6982.8W/m^(2) K](https://img.qammunity.org/2021/formulas/physics/college/xgpokpj66crwnfnt3kotps0xxxgq8ktfx9.png)
![Q_(T) =Ah(T_(plate) -T_(\alpha ) )=0.15*0.3*3982.8*(70-5)=17282.5W](https://img.qammunity.org/2021/formulas/physics/college/wyn03a3qcyg4mvawyly9sd5x4ewwmg0sft.png)