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Dennis_Churaev [7]
3 years ago
15

A heat engine has three quarters the thermal efficiency of a carnot engine operating between temperatures of 65°C and 435°C if

the heat engine absorbs heat at a rate of 44.0 kW, at what rate is heat exhausted?
Physics
1 answer:
const2013 [10]3 years ago
8 0

Answer:

The value is  P_e  =  31275.2 \  W

Explanation:

From the question we are told that

   The efficiency of the carnot engine is  \eta

    The efficiency of a heat engine is k =  \frac{3}{4}  *  \eta

    The operating temperatures of the carnot engine is  T_1  =  65 ^oC =338 \ K  to  T_2 = 435  ^oC = 708 \  K

    The rate at which the heat engine absorbs energy is  P =  44.0 kW  = 44.0 *10^{3} \  W

Generally the efficiency of the carnot engine is mathematically represented as

          \eta =  [ 1 - \frac{T_1 }{T_2}  ]

=>       \eta =  [ \frac{T_2 - T_1}{T_2} ]

=>       \eta = 0.3856

Generally the efficiency of the heat engine is

           k  =  \frac{3}{4} * 0.3856

=>        k  = 0.2892

Generally the efficiency of the heat engine is also mathematically represented as

          k  =  \frac{W}{P}

Here W is the work done which is mathematically represented as

        W =  P - P_e

Here P_e  is the heat exhausted

So

       k  =  \frac{P - P_e}{P}

=>    0.2892   =  \frac{44*10^{3} - P_e}{44*10^{3}}

=>   P_e  =  31275.2 \  W

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Explanation:

a)

When an object is in circular motion, the angular speed of the object is the rate of change of its angular position. In formula, it is given by

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The angular speed of an object in circular motion can also be written as

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v=29,960 km/h is the linear speed, converted into m/s,

v=8322 m/s

r=2925 km = 2.925\cdot 10^6 m is the radius of the orbit

Subsituting into eq(1), we find the angular speed of the spaceship:

\omega=\frac{8322}{2.925\cdot 10^6}=0.0028 rad/s

b)

When an object is in circular motion, its direction is constantly changing, therefore the object is accelerating; in particular, there is a component of the acceleration acting towards the  centre of the orbit: this is called centripetal acceleration, or radial acceleration.

The magnitude of the radial acceleration is given by

a_r=\omega^2 r

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\omega is the angular speed

r is the radius of the orbit

For the spaceship in the problem, we have

\omega=0.0028 rad/s is the angular speed

r=2925 km = 2.925\cdot 10^6 m is the radius of the orbit

Substittuing into the equation above, we find the radial acceleration:

a_r=(0.0028)^2(2.925\cdot 10^6)=23.68 m/s^2

c)

When an object is in circular motion, it can also have a component of the acceleration in the direction tangential to its motion: this component is called tangential acceleration.

The tangential acceleration is given by

a_t=\frac{\Delta v}{\Delta t}

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\Delta v is the change in the linear speed

\Delta  t is the time interval

In this problem, the spaceship is moving with constant linear speed equal to

v=8322 m/s

Therefore, its linear speed is not changing, so the change in linear speed is zero:

\Delta v=0

And therefore, the tangential acceleration is zero as well:

a_t=\frac{0}{\Delta t}=0 m/s^2

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