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Jet001 [13]
3 years ago
11

P1.30 shows a gas contained in a vertical piston– cylinder assembly. A vertical shaft whose cross-sectional area is 0.8 cm2 is a

ttached to the top of the piston. Determine the magnitude, F, of the force acting on the shaft, in N, required if the gas pressure is 3 bar. The masses of thepiston and attached shaft are 24.5kg and 0.5kg respectively. The piston diameter is 10cm. The local atmospheric pressure is 1 bar. The piston moves smoothly in the cylinder and g=9.81 m/s2
Engineering
1 answer:
iogann1982 [59]3 years ago
6 0

Answer:

1.737 kJ

Explanation:

Thinking process:

Step 1

Data:

Area of the shaft = 0.8 cm²

Combined mass of shaft and piston  = (24.5 + 0.5) kg

                                                             = 25 kg

Piston diameter                                   = 0.1 m

External atmospheric pressure          = 1 bar = 101.3 kPa

Pressure inside the gas cylinder      = 3 bar = 3 × 101.3 kPa

g                                                           = 9.81 m/s²

Step 2

Draw a free body diagram

Step 3: calculations

area of the piston = 0.0314 m²

Change in the elevation of the piston, \deltaz

\deltaz = \frac{PE}{mg}

    = \frac{0.2*10x^{3} }{25*9.81}

    = 0.82 m

Next, we evaluate the work done by the shaft:

W_{s} = F_{s} Z

     = (1668) ( 0.082)

     = 1. 37 kJ

Net area for work done = A (piston) - Area of shaft

                                       = \pi*(0.1)^{2}  - 0.8 cm^{2}

                                        = 77.7 cm²

                                        = 0.007774 m²

Work done in overcoming atmospheric pressure:

 Wₐ = PAZ

       =101.3 kPa * 0.007774 * 0.82

      =  0.637 kJ

total work = work done by shaft + work to overcome atmospheric pressure = 0.367 + 1.37

= 1.737 kJ Ans

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Answer:

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                     T_2 = T_1 * r^(k-1/k)

                     T_2 = T_4 = T_10 = 520*3^(.4/1.4) = 711.744 R

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                     T_7 = T_6 * r^(-k-1/k)

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- The mass flow rate is obtained by:

                     flow(m) = W_net,out / 2*c_p*(1400-1022.84-711.744+520)

                     flow(m) = 1000*.7068 / 2*0.24*(1400-1022.84-711.744+520)

                     flow(m) = 7.941 lbm/s

- The heat input is as follows:

                     Q_in = c_p*(T_6 - T_5)

                     Q_in = 0.24*(1400 - 1022.84)

                     Q_in = 90.5184 Btu/lbm

- The heat output is as follows:

                     Q_out = c_p*(T_10 - T_1)

                     Q_out = 0.24*(711.744 - 520)

                    Q_out = 56.01856 Btu/lbm

                                           

                     

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Explanation:

Given Data:

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height = 200mm ;

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Now, as we know that force per unit area equals to stress

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First we need to calculate total area,

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By putting the values in equation 1, we get

P/40000 = 620 * 0.01

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