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choli [55]
3 years ago
9

Pressurized steam at 400 K flows through a long, thin- walled pipe of 0.6-m diameter. The pipe is enclosed in a concrete casing

that is of square cross section and 1.75 m on a side. The axis of the pipe is centered in the casing, and the outer surfaces of the casing are maintained at 300 K. What is the rate of heat loss per unit length of pipe
Engineering
2 answers:
ELEN [110]3 years ago
7 0

Explanation:

assume steady state conditions, negligible steam side convention resistance, pipe wall resistance and contact resistance i.e T_{1} =400k

and constant properties of concrete (300 k); k=1.4Wm/k

the heat rate can be expressed as

q=Sk(T_{1} -T_{2} )=Ak(T_{1} -T_{2} )

the shape factor is

S=(2\pi L/ln(1.08w/D))

hence \\q'=q/L\\=2\pi k(T_{1}- T_{2}) /ln(1.08w/D)

insert values

=(2\pi *1.4W/m.k*(400-300)k)/(ln(1.08*1.75/0.6)

q'=766W/m   ( rate of heat loss per unit length)

Stels [109]3 years ago
6 0

Answer:

Q= 930.92W/m

Explanation:

Note that thermal conductivity of some common materials is from engineering tool box.

And the proper shape factor needed for the solution is found from the List of shape factor

Pressure of steam(T1)=400k

Diameter of the pipe(D)=0.6m

Square cross section of the concrete casing (W) =1.75m

Outer surface of casting maintained at a pressure (T2)=300k

Thermal conductivity (K) =1.7W/mK

The proper shape factor needed for the solution is found from the List of shape factor

Rate of heat loss (Q) =?

The heat rate (q) :

q=SKΔT1-T2=SK(T1-T2)

S=2πL/In(1.08W/D)

Heat loss per unit length is in terms of W/M

Note that, Q=q/L

By substitution, the full equation will be

Q=2πK(T1-T2)/In(1.08W/D)

Substituting values :

Q=2π(1.7W/mK)*(400K - 300k) / In[ (1.08(1.75m)/ 0.6m ]

Q= 930.92W/m

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A car is traveling at sea level at 78 mi/h on a 4% upgrade before the driver sees a fallen tree in the roadway 150 feet away. Th
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Answer: V = 47.7 mi/hr

Explanation:

first we calculate elements of aero-dynamic resistance

Ka = p/2 * CD * A.f

p is the density of air(0.002378 slugs/ft^3) for zero altitude, CD is the drag coefficient(0.35) and A.f is the front region of the vehicle

so we substitute

Ka = 0.002378/2 * 0.35 * 18

Ka = 0.00749

Now we calculate the final speed of the vehicle (V2) using the relation;

S = (YbW/2gKa)In[ (UW + KaV1^2 + FriW ± Wsinθg) / (UW + KaV2^2 + FriW ± Wsinθg)

so

WE SUBSTITUTE

150 = (1.04 * 2700 / 2 * 32.2 * 0.0075) In [(0.8 * 2700 + 0.0075 *(78mil/hr * 5280ft/1min * 1hr/3600s)^2 + 0.017 * 2700 ± 2700 * 0.04) / (0.8 * 2700 + 0.0075 * V2^2 + 0.017 * 2700 ± 2700 * 0.04)]

150 = (2808/0.483) In [(2160 + 98.16 + 153.9) / ( 2160 + 0.0075V2^2 + 153.9)]

150 = 5813.66 In [ (2160 + 98.16 + 153.9) / ( 2160 + 0.0075V2^2 + 153.9)]

divide both sides by 5813.66

0.0258 = In [ (2412.06) / ( 0.0075V2^2 + 2313.9)]

take the e^ of both side

e^0.0258 = (2412.06) / ( 0.0075V2^2 + 2313.9)

1.0261 = (2412.06) / ( 0.0075V2^2 + 2313.9)]

(0.0075V2^2 + 2313.9) = 2412.06 / 1.0261

(0.0075V2^2 + 2313.9) = 2350.7

0.0075V2^2 = 2350.7 - 2313.9

0.0075V2^2 = 36.8

V2^2 = 36.8 / 0.0075

V2^2 = 4906.6666

V2 = √4906.6666

V2 = 70.0476 ft/s

converting to miles per hour

V2 = 70.0476 ft/s * 1 mil / 5280 ft * 3600s / 1hr

V = 47.7 mi/hr

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Is the COP of a heat pump always larger than 1?
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Answer:

Yes

Explanation:

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