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avanturin [10]
3 years ago
11

Air at 80 kPa and 10°C enters an adiabatic diffuser steadily with a velocity of 150 m/s and leaves with a low velocity at a pre

ssure of 100 kPa. The exit area of the diffuser is 5 times the inlet area. Determine: i. the exit temperature of the air, and ii. the exit velocity of air.
Engineering
1 answer:
il63 [147K]3 years ago
7 0

Answer:

The exit temperature is 293.74 K.

Explanation:

Given that

At inlet condition(1)

P =80 KPa

V=150 m/s

T=10 C

Exit area is 5 times the inlet area

Now

A_2=5A_1

If consider that density of air is not changing from inlet to exit then by using continuity equation

A_1V_1=A_2V_2

So   A_1\times 150=5A_1V_2

V_2=30m/s

Now from first law for open system

h_1+\dfrac{V_1^2}{2}+Q=h_2+\dfrac{V_2^2}{2}+w

Here Q=0 and w=0

h_1+\dfrac{V_1^2}{2}=h_2+\dfrac{V_2^2}{2}

When air is treating as ideal gas  

h=C_pT

Noe by putting the values

h_1+\dfrac{V_1^2}{2}=h_2+\dfrac{V_2^2}{2}

1.005\times 283+\dfrac{150^2}{2000}=1.005\times T_2+\dfrac{30^2}{2000}

T_2=293.74K

So the exit temperature is 293.74 K.

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52m/s

12 kpa

0.1 kg/m

Explanation:

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6 0
2 years ago
Air enters a compressor at a pressure of 74.7 kPa and 287 K and leaves at 622 kPa and 579 K. The air flow rate is 50 kg/s. Calcu
vampirchik [111]

Answer:

attached below

Explanation:

7 0
2 years ago
A square aluminum plate 5 mm thick and 150 mm on a side is heated while vertically suspended in quiescent air at 75°c. determine
Doss [256]

By using the boundary layer equation, the average heat transfer coefficient for the plate is equal to 4.87 W/m²k.

<u>Given the following data:</u>

Surface temperature = 15°C

Bulk temperature = 75°C

Side length of plate = 150 mm to m = 0.15 meter.

<h3>How to calculate the average heat transfer coefficient.</h3>

Since we have a quiescent room air and a uniform pole surface temperature, the film temperature is given by:

T_f=\frac{T_{s} + T_{\infty} }{2} \\\\T_f=\frac{15 + 75 }{2} \\\\T_f = 45

Film temperature = 45°C to K = 273 + 45 = 318 K.

For the coefficient of thermal expansion, we have:

\beta =\frac{1}{T_f} \\\\\beta =\frac{1}{318}

From table A-9, the properties of air at a pressure of 1 atm and temperature of 45°C are:

  • Kinematic viscosity, v = 1.750 \times 10^{-5} m²/s.
  • Thermal conductivity, k = 0.02699 W/mk.
  • Thermal diffusivity, α = 2.416 \times 10^{-5} m²/s.
  • Prandtl number, Pr = 0.7241.

Next, we would solve for the Rayleigh number to enable us determine the heat transfer coefficient by using the boundary layer equations:

R_{aL}=\frac{g\beta \Delta T l^3}{v\alpha } \\\\R_{aL}=\frac{9.8 \;\times \;\frac{1}{318} \;\times \;(75-15) \;\times \;0.15^3 }{1.750 \times 10^{-5}\; \times \;2.416 \times 10^{-5} } \\\\R_{aL}=\frac{9.8\; \times 0.00315 \;\times \;60\; \times\; 0.003375 }{4.228 \times 10^{-10}  }\\\\R_{aL}=1.48 \times 10^{7}

Also take note, g(Pr) is given by this equation:

g(P_r)=\frac{0.75P_r}{[0.609 \;+\;1.221\sqrt{P_r}\; +\;1.238P_r]^\frac{1}{4} } \\\\g(P_r)=\frac{0.75(0.7241)}{[0.609 \;+\;1.221\sqrt{0.7241}\; +\;1.238(0.7241)]^\frac{1}{4} }\\\\g(P_r)=\frac{0.543075}{[0.609 \;+\;1.221\sqrt{0.7241}\; +\;1.238(0.7241)]^\frac{1}{4} }\\\\g(P_r)=\frac{0.543075}{[2.5444]^\frac{1}{4} }\\\\g(P_r)=\frac{0.543075}{1.2630 }

g(Pr) = 0.430

For GrL, we have:

G_{rL}=\frac{R_{aL}}{P_r} \\\\G_{rL}=\frac{1.48 \times 10^7}{0.7241} \\\\G_{rL}=1.99 \times 10^7

Since the Rayleigh number is less than 10⁹, the flow is laminar and the condition is given by:

N_{uL}=\frac{h_{L}L}{k} = \frac{4}{3} (\frac{G_{rL}}{4} )^\frac{1}{4} g(P_r)\\\\h_{L}=\frac{0.02699}{0.15} \times  [\frac{4}{3} \times  (\frac{1.99 \times 10^7}{4} )^\frac{1}{4} ]\times 0.430\\\\h_{L}= 0.1799 \times 62.9705 \times 0.430\\\\h_{L}=4.87\;W/m^2k

Based on empirical correlation method, the average heat transfer coefficient for the plate is given by this equation:

N_{uL}=\frac{h_{L}L}{k} =0.68 +  \frac{0.670 R_{aL}^\frac{1}{4}}{[1+(\frac{0.492}{P_r})^\frac{9}{16}]^\frac{4}{19}   } \\\\h_{L}=\frac{0.02699}{0.15} \times ( 0.68 +  \frac{0.670 (1.48 \times 10^7)^\frac{1}{4}}{[1+(\frac{0.492}{0.7241})^\frac{9}{16}]^\frac{4}{19}   })\\\\h_{L}=4.87\;W/m^2k

Read more on heat transfer here: brainly.com/question/10119413

3 0
2 years ago
given two continuous time signals x(t) and h(t), if their convultion is denoted by y(t) , then the convultion of x(t-1) and h(t+
goldenfox [79]

Answer:

y(t)=h(t+1)*x(t-1)

Explanation:

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3 0
3 years ago
Aggregate blend composed of 65% coarse aggregate (SG 2.701), 35% fine aggregate (SG 2.625)
dimaraw [331]

Answer:

  • 2.674
  • 2.428
  • 91.695%
  • 2.592
  • 3.305%
  • 11.786%
  • 78.1%

Explanation:

coarse aggregate (ca) = 65%,   SG = 2.701

Fine aggregate = 35%,    SG = 2.625

A) Bulk specific gravity of aggregate

   = \frac{65*2.701 + 35*2.625}{100}  = 2.674

B) Wm = 1257.9 g { weight in air }

    Ww = 740 g { submerged weight }

   therefore Bulk specific gravity of compacted specimen

   = \frac{Wm}{Wm-Ww}  =  \frac{1257.9}{1257.9 - 740 }  =  2.428

   Theoretical specific gravity = 2.511

Percent stone

= 100 - asphalt content - Vv

= 100 - 5 - 3.305 = 91.695%

c) percent of void

= \frac{9.511-2.428}{2.511} * 100    Vv = 3.305%

d) let effective specific gravity in stone

     = \frac{91.695*unstone+ 5 *1.030 }{96.695} = 2.511

    = Instone = 2.592 effective specific gravity of stone

e) Vv = 3.305%

f ) volume filled with asphalt (Vb) = \frac{\frac{Wb}{lnb} }{\frac{Wm}{Inm} } * 100

           Vb = \frac{5 * 2.428}{1.030 * 100} * 100

          Vb = 11.786 %

Volume of mineral aggregate = Vb + Vv

              VMA = 11.786 + 3.305 = 15.091

g) percent void filled with alphalt

     = Vb / VMA * 100

    VMA = 11.786 + 3.305 = 15.091

   percent void filled with alphalt

     = Vb / VMA * 100 = (11.786 / 15.091) * 100 = 78.1%

 

3 0
2 years ago
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