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Sedbober [7]
3 years ago
13

Can I have free money? I want to get a new pc

Engineering
2 answers:
GREYUIT [131]3 years ago
6 0

Answer:

NO!

Explanation:

Salsk061 [2.6K]3 years ago
3 0

Answer:

Money isnt free sorry i wish i had free money also

Explanation:

You might be interested in
A heat exchanger takes compressed liquid water and converts it into steam with a temperature and pressure of 20 Mpa and 480 C; r
belka [17]

Answer:

See explaination

Explanation:

Lets first consider the term Isentropic efficiency. The isentropic efficiency of a compressor or pump is defined as the ratio of the work input to an isentropic process, to the work input to the actual process between the same inlet and exit pressures. IN practice, compressors are intentionally cooled to minimize the work input.

Please kindly check attachment for the step by step solution of the given problem.

6 0
3 years ago
A horizontal opaque flat plate is well insulated on the edges and the lower surface. The top surface has an area of 8 m2 and it
Oliga [24]

Answer:

a = 0.8333

p = 0.1667

ε = 0.6243        

Explanation:

Given:

- Solar Irradiation G = 6000 W

- Irradiation absorbed G_abs = 5000 W

- Heat Loss by convection Q_convec = 750 W

- The temperature of surface remains constant @ 350 K

Find:

Determine the absorptivity, reflectivity, and emissivity of the plate

Solution:

- Absorptivity is the ratio of energy absorbed to the incident energy given as:

                                        a = G_abs / G

- Plug in values:              a = 5000 / 6000

                                        a = 0.8333

- Reflectivity is the ratio of energy not absorbed to the incident energy given as:

                                          p = (1 - G_abs) / G

- Plug in values:                p = 1000 / 6000

                                          p = 0.1667

- Emissivity is the of ratio amount energy that is radiated from the body to the black body:

- We will use energy balance on the plate surface:

                                          E_in - E_out = -k*A*dT / L

- We know that the plate temperature remains constant, dT = 0:

                                          E_in = E_out

                                          Q_abs = Q_convec + Q_rad

                                          Q_rad = Q_abs - Q_convec

- Plug in values:                Q_rad = 5000 -  750 = 4250 W

- The expression for surface radiation is given by:

                                           Q_rad = ε*A*б*T_b^4

- Re-arrange:                     ε = Q_rad / A*б*T_b^4  

- Plug values in:                ε = 4250 / 8*(5.67*10^-8)*(350)^4    

                                           ε = 0.6243        

4 0
3 years ago
Four important biogeochemical cycle<br>​
olga55 [171]

Answer:

The four important biogeochemical cycle are:

1 Water Cycle or Hydrologic Cycle

2 Carbon-Cycle

3 Nitrogen Cycle

4 Oxygen Cycle.

3 0
3 years ago
Read 2 more answers
⦁ An ideal Otto cycle has a compression ratio of 8. At the beginning of the compression process, air is at 95 kPa and 27°C, and
Anon25 [30]

Answer:

<u><em>note:</em></u>

<u><em>solution is attached in word form due to error in mathematical equation. furthermore i also attach Screenshot of solution in word due to different version of MS Office please find the attachment</em></u>

Download docx
8 0
4 years ago
Steam enters an adiabatic nozzle at 2.5 MPa and 450oC with a velocity of 55 m/s and exits at 1 MPa and 390 m/s. If the nozzle ha
luda_lava [24]

Answer:

The value of exit temperature from the nozzle = 719.02 K

Explanation:

Temperature at inlet T_{1} = 450°c = 723 K

Velocity at inlet V_{1} = 55 \frac{m}{sec}

velocity at outlet V_{2} = 390 \frac{m}{sec}

Specific heat at constant pressure for steam  C_{p}  = 18723 \frac{J}{kg k}

Apply steady flow energy equation for the nozzle

h_{1} + \frac{V_{1} ^{2} }{2} = h_{2} + \frac{V_{2} ^{2} }{2}

C_{p} T_{1}  + \frac{V_{1} ^{2} }{2} = C_{p} T_{2} + \frac{V_{2} ^{2} }{2}

Put all the values in the above formula we get,

⇒ 18723 × 723 + \frac{55^{2} }{2} = C_{p} T_{2} + \frac{390^{2} }{2}

⇒   T_{2} = 719.02 K

This is the value of exit temperature from the nozzle.

4 0
4 years ago
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