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Katen [24]
3 years ago
11

A flocculation basin equipped with revolving paddles is 60 ft long (the direction of flow). 45 ft wide, and 14 ft deep and treat

s 10 mgd. The power input to provide paddle-blade velocities of 1.0 and 1.4 fps for the inner and outer blades, respectively, is 930 ft'lb/s. Calculate the detention time, horizontal flow-through velocity, and G (the mean velocity gradient) for a water temperature of 50'F.
Engineering
1 answer:
Vinil7 [7]3 years ago
6 0

Answer:

detention time =  40.72 minutes

horizontal velocity v  = 0.295 inch/s

mean velocity gradient, G = 54.38 s^{-1}

Explanation:

given data

long = 60 ft

wide = 45 ft

deep = 14 ft

flow of water to treat = 10 mgd = 15.472 ft³/s         [1 MGD = 1.5472 ft³/s ]

inner velocities = 1.0  fps

outer velocities = 1.4  fps

power required to rotates the paddles = 930 ft-lb/s

solution

we find detention time that is

time = \frac{V}{Q}

here  Q = flow of water and  V is volume of water

so

volume of flocculation basin is = 60 × 45 × 14 = 37800 ft³

so

detention time = \frac{37800}{15.472}

detention time =  40.72 minutes

and

horizontal flow through velocity is

cross-section area of tank = 45 × 14 = 630 ft²

and we know that  Av = Q

so horizontal velocity v =  \frac{Q}{A}

horizontal velocity v =  \frac{15.472}{630}

horizontal velocity v = 0.02456 ft/s

horizontal velocity v  = 0.295 inch/s

and

now we find mean velocity gradient G at  temperature of 50'F

so formula is G = \sqrt{\frac{P}{\mu V} }      

here P is power input  and μ is  viscosity  and V is  volume of flocculation basin

so Volume of flocculation basin is 37800 ft³

and μ for 500F = 8.3197  × 10^{-6} lb-s/ft²

we take from table

so we get

G = \sqrt{\frac{930}{8.3197*10^{-6}*37800} }  

mean velocity gradient, G = 54.38 s^{-1}

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Answer:

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Explanation:

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Now from the question,

L = 4m

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So Area will be A_2 - A_1

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We are given that;

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R = 4/(2 x 10^(-4) x 6.28x 10^(-4))

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3 years ago
Air at 400kPa, 970 K enters a turbine operating at steady state and exits at 100 kPa, 670 K. Heat transfer from the turbine occu
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Answer:

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     From  the question we are told

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the negative sign because the heat is transferred from the turbine

          The specific heat capacity of air is c_p = 1.1KJ/kg \cdot K

          The inlet temperature is  T_1 = 970K

          The outlet temperature is T_2 = 670K

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          The pressure at the exist of the turbine is p_2 = 100kPa

           The temperature at outer surface is T_s = 315K

         The individual gas constant of air  R with a constant value R = 0.287kJ/kg \cdot K

The general equation for the turbine operating at steady state is \

               \r Q - \r W + \r m (h_1 - h_2) = 0

h is the enthalpy of the turbine and it is mathematically represented as          

        h = c_p T

The above equation becomes

             \r Q - \r W + \r m c_p(T_1 - T_2) = 0

              \frac{\r W}{\r m}  = \frac{\r Q}{\r m} + c_p (T_1 -T_2)

Where \r Q is the heat transfer from the turbine

           \r W is the work output from the turbine

            \r m is the mass flow rate of air

             \frac{\r W}{\r m} is the rate of work developed

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              \frac{\r W}{\r m} =  (-30)+1.1(970-670)

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The general balance  equation for an entropy rate is represented mathematically as

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          =>          \frac{\sigma}{\r m} = - \frac{\r Q}{\r m T_s} + (s_1 -s_2)

    generally (s_1 -s_2) = \Delta s = c_p\ ln[\frac{T_2}{T_1} ] + R \ ln[\frac{v_2}{v_1} ]

substituting for (s_1 -s_2)

                      \frac{\sigma}{\r m} = \frac{-\r Q}{\r m} * \frac{1}{T_s} +  c_p\ ln[\frac{T_2}{T_1} ] - R \ ln[\frac{p_2}{p_1} ]

                      Where \frac{\sigma}{\r m} is the rate of entropy produced within the turbine

 substituting values

                \frac{\sigma}{\r m} = - (-30) * \frac{1}{315} + 1.1 * ln\frac{670}{970} - 0.287 * ln [\frac{100kPa}{400kPa} ]

                    \frac{\sigma}{\r m}=  0.0861kJ/kg \cdot K

           

 

                   

   

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