\(1.2 \mathrm{~kg}\) of liquid water initially at \(15^{\circ} \mathrm{C}\) is to be heated to \(95^{\circ} \mathrm{C}\) in a teapot equipped with a \(1200-\mathrm{W}\) electric heating element inside. The teapot is \(0.5 \mathrm{~kg}\) and has an average specific heat of \(0.7 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\). Taking the specific heat of water to be \(4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\) and disregarding any heat loss from the teapot, determine how long it will take for the water to be heated.

Short Answer

Expert verified
Based on the given information, it takes about 6 minutes to heat the water in the teapot from 15°C to 95°C using a 1200 W electric heating element. This is determined by calculating the heat energy required for both the water and the teapot and dividing the total heat energy by the power of the heating element.

Step by step solution

01

Calculate the heat energy required to heat the water

First, we need to determine the heat energy absorbed by the water. We can do this using the formula: \(Q_{water} = m_{water} \times c_{water} \times (\Delta T_{water})\) Where: - \(Q_{water}\) is the heat energy absorbed by the water - \(m_{water}\) is the mass of the water (\(1.2 \mathrm{~kg}\)) - \(c_{water}\) is the specific heat capacity of water (\(4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\)) - \(\Delta T_{water}\) is the temperature difference experienced by the water (80°C) We can now plug in the values and calculate the heat energy required to heat the water: \(Q_{water} = 1.2 \mathrm{~kg} \times 4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K} \times 80 \mathrm{~K} = 402.048 \mathrm{~kJ}\)
02

Calculate the heat energy required to heat the teapot

Similarly, we now need to determine the heat energy absorbed by the teapot using the formula: \(Q_{teapot} = m_{teapot} \times c_{teapot} \times (\Delta T_{teapot})\) Where: - \(Q_{teapot}\) is the heat energy absorbed by the teapot - \(m_{teapot}\) is the mass of the teapot (\(0.5 \mathrm{~kg}\)) - \(c_{teapot}\) is the specific heat capacity of the teapot (\(0.7 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\)) - \(\Delta T_{teapot}\) is the temperature difference experienced by the teapot (80°C) We can now plug in the values and calculate the heat energy required to heat the teapot: \(Q_{teapot} = 0.5 \mathrm{~kg} \times 0.7 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K} \times 80 \mathrm{~K} = 28 \mathrm{~kJ}\)
03

Calculate the total heat energy required

To find the total heat energy required to heat the water and the teapot, we simply add the heat energy required for each component: \(Q_{total} = Q_{water} + Q_{teapot} = 402.048 \mathrm{~kJ} + 28 \mathrm{~kJ} = 430.048 \mathrm{~kJ}\)
04

Calculate the heating time

Finally, we can find the time it takes for the water to be heated by dividing the total heat energy required by the power of the heating element. Note that we also need to convert the power from watts to kilowatts by dividing it by 1000: \(P = 1200 \mathrm{~W} = 1.2 \mathrm{~kW}\) Time \(t\) is given by: \(t = \frac{Q_{total}}{P} = \frac{430.048 \mathrm{~kJ}}{1.2 \mathrm{~kW}} = 358.373 \mathrm{~s}\) The water and the teapot will be heated to the desired temperature in approximately 358.373 seconds (or about 6 minutes).

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Most popular questions from this chapter

A 25 -cm-diameter black ball at \(130^{\circ} \mathrm{C}\) is suspended in air, and is losing heat to the surrounding air at \(25^{\circ} \mathrm{C}\) by convection with a heat transfer coefficient of \(12 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and by radiation to the surrounding surfaces at \(15^{\circ} \mathrm{C}\). The total rate of heat transfer from the black ball is (a) \(217 \mathrm{~W}\) (b) \(247 \mathrm{~W}\) (c) \(251 \mathrm{~W}\) (d) \(465 \mathrm{~W}\) (e) \(2365 \mathrm{~W}\)

How does forced convection differ from natural convection?

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The outer surface of a spacecraft in space has an emissivity of \(0.8\) and a solar absorptivity of \(0.3\). If solar radiation is incident on the spacecraft at a rate of \(950 \mathrm{~W} / \mathrm{m}^{2}\), determine the surface temperature of the spacecraft when the radiation emitted equals the solar energy absorbed.

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