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Vesna [10]
3 years ago
13

A source of heat at 1000 K transfers 1000 kW of power to a power generation device, while producing 400 kW of useful work. Deter

mine the second law efficiency of the system, if the environment is at 300 K.
Physics
1 answer:
Eva8 [605]3 years ago
4 0

Answer:

The value is \eta _2 = 0.57

Explanation:

From the question we are told that

    The temperature of the heat source is T_s =  1000 \  K

    The amount of power transferred is  P_s =  1000 \  kW =  1000 *10^{3} \  W

      The work produced is  W = 400 \  kW

       The temperature of the environment T_e  =  300 \  K

Gnerally the Carnot efficiency of the system is mathematically represented as

        \eta_c =  1 -\frac{T_e}{T_s}

=>    \eta_c = 1 -\frac{300}{1000}

=>      \eta_c =  0.7

Generally the first  law efficiency of the system is mathematically represented as

            \eta _1 = \frac{W}{P_s}

=>         \eta _1 = \frac{400}{1000}  

=>         \eta _1 = 0.40

Generally the second  law efficiency of the system is mathematically represented as

                \eta _2 = \frac{\eta_1}{\eta_c}

=>               \eta _2 = \frac{0.4}{0.7}

=>               \eta _2 = 0.57

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Answer:

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There are actually more ways to fill in those two blanks... Different parts of the body absorb x-rays in varying degrees, but soft tissues (like skin, muscles, fat, and organs) allow most of the X-rays to pass through.

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During a demonstration of the gravitational force on falling objects to her class, Sarah drops an 11 lb. bowling ball from the t
leonid [27]

The instant it was dropped, the ball had zero speed.

After falling for 1 second, its speed was 9.8 m/s straight down (gravity).

Its AVERAGE speed for that 1 second was (1/2) (0 + 9.8) = 4.9 m/s.

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A 10 kilogram lump of rock weighs 16N on the Moon.
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Suppose the rocket in the Example was initially on a circular orbit around Earth with a period of 1.6 days. Hint (a) What is its
ruslelena [56]

Answer:

a

The orbital speed is v= 2.6*10^{3} m/s

b

The escape velocity of the rocket is  v_e= 3.72 *10^3 m/s

Explanation:

Generally angular velocity is mathematically represented as

            w = \frac{2 \pi}{T}

Where T is the period which is given as 1.6 days = 1.6 *24 *60*60 = 138240 sec

       Substituting the value

         w = \frac{2 \pi}{138240}

             = 4.54*10^ {-5} rad /sec

At the point when the rocket is on a circular orbit  

   The gravitational force =  centripetal force and this can be mathematically represented as

              \frac{GMm}{r^2} = mr w^2

Where  G is the universal gravitational constant with a value  G = 6.67*10^{-11}

            M is the mass of the earth with a constant value of M = 5.98*10^{24}kg

            r is the distance between earth and circular orbit where the rocke is found

               Making r the subject

                     r = \sqrt[3]{\frac{GM}{w^2} }

                        = \sqrt[3]{\frac{6.67*10^{-11} * 5.98*10^{24}}{(4.45*10^{-5})^2} }

                        = 5.78 *10^7 m

The orbital speed is represented mathematically as

                   v=wr

Substituting value

                  v= (5.78*10^7)(4.54*10^{-5})

                     v= 2.6*10^{3} m/s    

The escape velocity is mathematically represented as

                            v_e = \sqrt{\frac{2GM}{r} }

Substituting values

                             = \sqrt{\frac{2(6.67*10^{-11})(5.98*10^{24})}{5.78*10^7} }

                             v_e= 3.72 *10^3 m/s

7 0
3 years ago
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