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3 Marks Question

Question 513 Marks
State first law of thermodynamics. Why $C_p > C_v$? Prove $C_p - C_v = R$.
Answer
First Law of Thermodynamics: It is based on the law of conservation of energy. The total heat energy change in any system is the sum of the internal energy change and the work done, i.e. dQ = dU + dW. where dU is the internal energy change and dW = PdV is the work done by/ on the system. $C_p$ is greater because under constant pressure process, the energy also does work. Poof of $C_p - C_v = R$ Suppose one mole of a gas is heated at constant volume so that its temperature rises by dT. Heat supplied = $1 × C_V \times dT = C_VsdT$ ...(i) Since the volume is constant, the gas will not perform external work in accordance with the first law of thermodynamics and the heat supplied will be just equal to the increase in the internal energy of the gas.
$\therefore dU = C_VdT$ ...(ii) Let the gas be heated at constant pressure to increase its temperature by dT, and dQ be the amount of heat supplied, therefore, $dQ = 1 \times C_P \times dT = C_PdT$ ...(iii) The heat supplied at a constant pressure increases the temperature by dT, hence increases its internal energy by $dU = C_vdT$ as well as enables the gas to perform work dW. dW = PDV ...(iv) From the first law of thermodynamics, we have, dQ = dU + dW Substituting the values, we get, $C_PdT = C_VdT + PdV$ But PV = RT (For one mole of an ideal gas) or PdV = RdT,
$\therefore\text{C}_\text{P}\text{dt}=\text{C}_\text{P}\text{dT}+\text{RdT} C_P - C_V = R$ ...(v) This is the relationship between two principal specific heats of the gas when $C_p, C_v$​​​​​​​ and R are measured in the units of either heat or of work.
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Question 523 Marks
Temperatures of the hot and cold reservoirs of a Carnot engine is raised by equal amounts. How the efficiency of the Carnot engine affected?
Answer
Let the initial temperatures of hot and cold reservoirs were $T_1$ and $T_2$. The efficiency of the Carnot engine is given by, So, intially $\eta=\frac{\text{T}_1-\text{T}_2}{\text{T}_1}\dots\text{(i)}$ As given the temperature of both the reservoirs is raised by equal amout t so $\text{T}'_1=\text{T}+\text{t}$ and $\text{T}'_2=\text{T}_2+\text{t}.$ The final efficiency of the Carnot engine will be $\eta'=\frac{\text{T}'_1-\text{T}_2'}{\text{T}'_1}$
$=\frac{(\text{T}_1+\text{t})-(\text{T}_2'+\text{t})}{\text{(T}_1+\text{t)}}$
$=\frac{\text{T}_1-\text{T}_2}{(\text{T}_1+\text{t})}\dots\text{(ii)}$ Dividing equation (ii) by equation (i), we have $\frac{\eta'}{\eta}=\frac{\Big(\frac{\text{T}_1-\text{T}_2}{\text{T}_1+\text{t}}\Big)}{\Big(\frac{\text{T}_1-\text{T}_2}{\text{T}_1}\Big){}}=\frac{\text{T}_1}{\text{T}_1+\text{t}}\dots\text{(iii)}$ As $\eta'<\eta,$ i.e. the effieciency of Cornot engine decreases.
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Question 533 Marks
A perfect Carnot engine utilizes an ideal gas. The source temperature is $500K$ and sink temperature is $375K$. If the engine takes $600K$ cal per cycle from the source, compute:
  1. The efficiency of the engine.
  2. Work done per cycle.
  3. Heat rejected to the sink per cycle.
Answer
Here $T_1 = 500K$ $T_2 = 375K Q_1 =$ Heat absorbed per cycle $= 600\  kcal$
  1.  
$\therefore$ Using the relation,
$\eta=1-\frac{\text{T}_2}{\text{T}_1},$ we get
$\eta=\frac{\text{T}_1-\text{T}_2}{\text{T}_1}$
$=\frac{500-375}{500}$
$=\frac{125}{500}=0.25$
$\eta\%=0.25\times100$
$=25\%$
  1. Let $W =$ work done per cycle
$\therefore$ Using the relation
$\eta=\frac{\text{W}}{\text{Q}_1},$ we get
$\text{W}=\eta\text{Q}_1=0.25\times600\text{ kcal}=150\text{ kcal}$
$=150\times10^3\times4.2\text{J}$
$=6.3\times10^5\text{J}$
  1. Let $Q_2 =$ Heat rejected to the sink
$\therefore$ Using the relation
$\text{W}=\text{Q}_1-\text{Q}_2,$ we get
$\text{Q}_2=\text{Q}_1-\text{W}$
$=600-150=450\text{ kcal}$
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Question 543 Marks
A Carnot's engine whose sink is at a temperature of 300K has an efficiency of 40%. By how much should the temperature of the source be increased so as to increase the efficiency to 60%?
Answer
Let T be the temperature of the source. $\frac{40}{100}=\frac{\text{T}-300}{\text{T}}$ or $\frac25=\frac{\text{T}-300}{\text{T}}$ T = 500K Let the temperature be increased by $\theta,$ therefore $\frac{60}{100}=\frac{(\text{T}+\theta)-300}{(\text{T}+\theta)}$ $\frac35=\frac{500+\theta-300}{500+\theta}$ $\theta=\frac{500}2=250\text{K}$
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Question 553 Marks
Consider a Carnot's cycle operating between $T_1=500 \mathrm{~K}$ and $T_2=300 \mathrm{~K}$ producing 1 kJ of mechanical work per cycle. Find the heat transferred to the engine by the reservoirs.
Answer
Efficiency of Carnot's engine $\mu=1-\frac{\text{T}_{2}}{\text{T}_{1}}$ Tempreature of source or reservior = $T_1 = 500K $
Tempreature of sink $T_2 = 300K$
 $\therefore\mu=1-\frac{\text{T}_{2}}{\text{T}_{1}}$
$\frac{\text{Output work}}{\text{Input work}(E)}=1-\frac{300}{500}$
$\frac{1000\text{J}}{\text{x}}=1-0.6$
$\text{x}=\frac{1000}{\text{x}}=0.4$
$\text{x}=\frac{1000}{0.4}=2500 \text{J} .$
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Question 563 Marks
What are isotherms? Explain the process of liquiefication using it.
Answer
Isotherms are P-V graphs drawn at same temperature. When pressure is increased, volume is reduced at constant temperature. Beyond certain level, the pressure remains same for certain reduction in volume and then the pressure increases sharply. As temperature is increased, the constant portion reduces and at a temperature called critical temperature, the flat portion is absent. In each isotherm, before the flat portion is reached, the substance is in gaseous state and beyond the flat portion, it is in the liquid state. During the flat portion of P-V graph, the gas is under liquefication and so both gaseous and liquid states co-exist. Beyond T. it is not possible to liquefy the gas whatever large the pressure may be.
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Question 573 Marks
During India-Pakistan war, a soldier discovered that his lead bullet just melted when stopped by an obstacle. Calculate the velocity of the bullet if its temp. was $47.6^{\circ} \mathrm{C}$. Given: melting point of lead $=327^{\circ} \mathrm{C}$. Specific heat of lead $=0.03 \mathrm{cal} \mathrm{g}^{-10} \mathrm{C}^{-1}$, latent heat of fusion of lead $=6 \mathrm{cal} \mathrm{g}^{-1}$ and $\mathrm{J}=4.2 \times 10^7 \mathrm{erg} \mathrm{~car}^{-1}$. Assume that no heat is lost.
Answer
Increase in temperature, $\theta=(327-47.6)^\circ\text{C}=279.4^\circ\text{C}$ Let m be the mass of the bullet. Heat required, $\text{Q}=\text{mS}\theta+\text{mL}$ or $\text{Q}=\text{m}(\text{S}\theta+\text{L})$ $=\text{m}(0.03\times279.4+6)$ $=14.38\text{m cal}$ Work done, $\text{W}=\frac12\text{mv}^2$ Where v is the velocity of bullet, Now, $\text{W}=\text{JQ}$ $\therefore\frac12\text{mv}^2=4.2\times10^7\times14.38\text{m}$ $\text{v}^2=2\times4.2\times10^7\times14.38$ $\text{v}=3.48\times10^4\text{cm s}^{-1}$
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Question 583 Marks
In a perfect Carnot's engine, the temperature of the source and the sink are $500K$ and $375K$ respectively. If the engine consumes $6 \times 10^5 cal$ per cycle, find $(i)$ the efficiency of the engine, $(ii)$ work done per cycle, and $(iii)$ the heat rejected to the sink per cycle.
Answer
  1. $\eta=\Big(1-\frac{\text{T}_2}{\text{T}_1}\Big)\times100$
$=\Big(1-\frac{375}{500}\Big)\times100=25\%$
  1. $\eta=\frac{\text{W}}{\text{Q}_1};$
$\text{W}=\eta\text{ Q}_1;\text{Q}_1=6000\times10^3\text{cal}$
$\text{W}=\frac{25}{100}\times600\times10^3\text{cal}$
$=150\times10^3\text{cal}=150\times10^3\times4.2\text{J}$
$=6.8\times10^5J($approx$)$
  1. $\text{W}=\text{Q}_1-\text{Q}_2;\text{Q}_2=\text{Q}_1-\text{W}$
$=600\times10^3-150\times10^3$
$=45\times10^4$
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Question 593 Marks
A Carnot engine absorbs 1000J of heat energy from a reservoir at 12.7°C and rejects 600J of heat energy during each cycle. Calculate. (i) efficiency of the engine, (ii) temperature of sink, (iii) amount of useful work done per cycle.
Answer
Here, $\text{Q}-1=1000\text{J},\text{Q}_2=600\text{J},$ $\text{T}_1=127^\circ\text{C}=127+273=400\text{K}$ $\eta=?,\ \text{T}_2=?,\ \text{W}=?$ From $\frac{\text{Q}_2}{\text{Q}_1}=\frac{\text{T}_2}{\text{T}_2},\text{T}_2=\frac{\text{Q}_2}{\text{Q}_1}\times\text{T}_1$ $\text{T}_2=\frac{600}{1000}\times400=240\text{K}$ $=240-273=-33^\circ\text{C}$ $\eta=1-\frac{\text{T}_2}{\text{T}_1}=1-\frac{240}{400}=0.4=40\%$ Also, $\text{W}=\text{Q}_1-\text{Q}_2=1000-600=400\text{J}$
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Question 603 Marks
What is the Internal energy in the process of vapourisation?
Answer
During vapourisation, volume increases. So work done $=P\left(V_f-V_i\right)$ and temperature does not change. So, $d Q=m L_v$
$\therefore$ from first law of thermodynamics, $d U=d Q-D W=m L_v-P\left(V_f-V_i\right)$.
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Question 613 Marks
Show that an adiabatic curve is always steaper than an isothermal curve.
Answer
For Isothermal process, since PV = constant$\frac{\text{dP}}{\text{P}}=\frac{\text{dV}}{\text{V}}$
But for an adiabatic process, since
$\text{PV}^\gamma=\text{constant},\frac{\text{dP}}{\text{P}}=-\gamma\frac{\text{dV}}{\text{V}}$
So P-V graph is steaper for adiabatic process.
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Question 623 Marks
Two thermometers are constructed in the same way except that one has a spherical bulb and the other has an elongated cylindrical bulb. Which one will respond quickly to the temperature changes? Why?
Answer
Thermometer with the cylindrical bulb. It is because the area of a cylinderical surface is greater than a spherical surface. Therefore, mercury in the cylindrical bulb reaches the temperature of the surrounding earlier.
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Question 633 Marks
State law of equi-partition of energy. Use this law to calculate specific heats of monoatomic, diatomic and triatomic gases.
Answer
According to the equi partition of energy, each degree of freedom will contribute an equal energy of $\frac12\text{R}$ per mole. In mono, di and triatomic gases hawing 3, 5 and 6 or 7 degrees of freedom, the internal energy will be $\frac32\text{R},\frac52\text{RT}$ and $\frac62\text{RT}$ or $\frac72\text{RT}.$ Using dU = $nC_VdT$ for mole, we get $\text{C}_\text{V}=\frac32\text{R},\frac{5}{2}\text{R},$ and 3R or $\frac72\text{R}$ for the three gases respectively.
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Question 643 Marks
What are 'Super heated water' and 'Super cooled vapour'?
Answer
Water in liquid phase at a temperature above 100°C and a pressure more than 1atm is called as super heated water. In a pressure cooker, water is heated at a pressure more than 1atm and temperature above 100°C. Steam below temperature 100°C is called super-cooled vapour.
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Question 653 Marks
Let the temperatures $T_1$ and $T_2$ of the two heat reservoirs in an ideal Carnot engine be $1500^{\circ} \mathrm{C}$ and $500^{\circ} \mathrm{C}$ respectively. Which of these, increasing $T_1$ by $100^{\circ} \mathrm{C}$ or decreasing $T_2$ by $100^{\circ} \mathrm{C}$, would result in a greater improvement in the efficiency of the engine?
Answer
The efficiency of Carnot engine is given by, $\eta=1-\frac{\text{T}_2}{\text{T}_1}=\frac{\text{T}_1-\text{T}_2}{\text{T}_1}$
  1. When $T,$ is increased from $1500^\circ C$ to $1600^\circ C$ or $1600 + 273 = 1873K$ and $T,$ remains constant i.e., $500^\circ C$, or $500 + 273 = 773K$, then
$\eta_1=\frac{1873-773}{1873}=\frac{1100}{1873}$
$=\frac{1100\times100}{1873}=58.73\%$
  1. When $T_1$ remains constant i.e., $1500^\circ C$ or $1500 + 273 = 1773K$ and $T_2$ is decreased by $100 ^\circ C$ i.e., from $500^\circ C$ to $400^\circ C$ or $400 + 273 = 673K$ then
$\eta_2=\frac{1773-673}{1773}=\frac{1100}{1773}$
$=\frac{1100\times100}{1773}=62.04\%$
Thus, $\eta_2>\eta_1$ Hence efficiency will be increased if $T_2$ is decreased from $500^\circ C$ to $400^\circ C.$
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Question 663 Marks
No real engine can have efficiency greater than that of a Carnot engine working between the same two temperatures, why?
Answer
A Carnot engine is an ideal heat engine from the following points of view:
  1. There is absolutely no friction between the walls of cylinder and the piston.
  2. The working substance is an ideal gas. In a real engine, these conditions cannot be fulfilled and hence no heat engine working between the same two temperatures can have efficiency greater than that of Carnot engine.
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Question 673 Marks
Calculate the efficiency of a Carnot's engine working between steam point and ice point.
Answer
Here, steam point, $\text{T}_1=100\ ^\circ\text{C}$ $=100+273=373\text{K}$ Ice point , $\text{T}_2=0^\circ{\text{C}}$ $=0+273=273\text{K}$ As $\eta=1-\frac{\text{T}_2}{\text{T}_1}$ $\therefore\ \eta=1-\frac{273}{373}=\frac{100}{373}$ $=\frac{100}{373}\times100\%$ $=26.81\%$
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Question 683 Marks
The temperature of equal masses of three different liquids $\mathrm{A}, \mathrm{B}$ and C are $12^{\circ} \mathrm{C}, 19^{\circ} \mathrm{C}$ and $28^{\circ} \mathrm{C}$ respectively. The temperature when A and B are mixed is $16^{\circ} \mathrm{C}$. When B and C are mixed, the temperature is $23^{\circ} \mathrm{C}$. What would be the temperature when A and C are mixed?
Answer
Let $S_A, S_B, S_C$ be the specific heats of liquids A, B and C respectively. When A and B are mixed, $\text{mS}_{\text{A}}(16-12)=\text{mS}_\text{B}(19-16)$
$\text{S}_\text{A}=\frac34\text{S}_\text{B}\dots\text{(i)}$ When B and C are mixed, $\text{ms}_\text{B}(23-19)=\text{mS}_\text{C}(28-23)$
$\text{S}_\text{B}=\frac{5}{4}\text{S}_\text{C}\dots\text{(ii)}$ From (i) and (ii), $\text{S}_\text{A}=\frac{15}{16}\text{S}_\text{C}$ Substituting in (iii), we get $\frac{15}{16}(\theta-12)\text{S}_\text{C}=(28-\theta)\text{S}_\text{C}$ or $\theta=22.0^\circ\text{C}.$
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Question 693 Marks
What is a heat engine? What is the best way to increase efficiency of a heat engine? Is it possible to design a thermal engine that has $100\%$ efficiency?
Answer
A heat engine is a device (or a combination) which converts heat into work. Its efficiency, $\eta=\frac{\text{Work output}}{\text{Heat input}}$
$\eta=1-\frac{\text{T}_2}{\text{T}_1}$ Where, $T_2$ = temperature of sink $T_1$ = temperature of source. From above expression, we can see that for 100% efficiency, $T_2 = 0$ It is impossible to design a thermal engine that has 100% efficiency because it is not possible to have a sink with kelvin temperature.
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Question 703 Marks
  1. Describe a Carnot's cycle.
  2. A thermodynamic system is taken from an original state to an intermediate state by the linear process shown in below figure. Its volume is then reduced to the original value from $E$ to $F$ by an isobaric process. Calculate the work done by the gas from $D$ to $E$ to $F$.
Answer
  1. Sadi Carnot devised an ideal cycle of operation of heat engine, which came to be known as Carnot cycle which is a set of four devices- a source at a high temperature (say $T_1$), a sink at a low temperature (say $T_2$), a non-conducting base and a cylinder with a working substance (a perfect gas) frictionless piston made of conducting base and non-conducting walls and piston.
  1. Change in pressure, $dP = 5.0 - 2.0\ atm = 3.0 \times 10^5 Nm^{-2}$​​​​​​​
Change in volume $dV = 600 - 300 = 300\ cc = 300 \times 10^{-6} m^3$
Work done by the gas from D to E to F
= Area of $\Delta\text{DEF}$
$=\frac{1}{2}\times\text{dP}\times\text{dV}$
$=\frac12\times3.0\times10^5\times300\times10^{-6}\text{m}^3$
$=45\times10^6\times10^{-6}=45\text{J}$
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Question 713 Marks
A Carnot engine whose heat sink is at $27°C$ has an efficiency of $40\%$. By how many degrees should the temperature of source be changed to increase the efficiency by $10\%$ of the original efficiency?
Answer
Here, $T_2 = 27^\circ C = 27 + 273 = 300K \eta=40\%,\text{ T}_2=?$ From, $\eta=1-\frac{\text{T}_2}{\text{T}_1}$
$\frac{\text{T}_2}{\text{T}_1}=1-\eta$
$=1-\frac{40}{100}$
$=\frac{60}{100}$
$=\frac35$
$\text{T}_1=\frac53\text{t}_2$
$=\frac{5}{3}\times300=500\text{K}$ Increase in efficiency = 10% of 40 = 4% Let $\text{T}_1'$ be the new temprature of the source. As $\eta'=1-\frac{\text{T}_2}{\text{T}'_1},$
$\therefore\frac{\text{T}_2}{\text{T}'_1}=1-\eta'$
$=1-\frac{44}{100}$
$=\frac{56}{100}$
$\text{T}'_1=\frac{100}{56}$
$\text{T}_2=\frac{100}{56}\times300$
$=535.7\text{K}$
$\therefore$ Increase in temperature of source = 535.7 - 500 = 35.7K
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Question 723 Marks
A gram molecule of a gas at $127°C$ expands isothermally until its volume is doubled. Find the amount of work done and heat absorbed.
Answer
Here, temperature of the gas, T=273 + 127 = 400 K Let initial volume of the gas, $V_1 = V $
$\therefore$ Final volume of the gas, $V_2 = 2V$ In an isothermal expansion, Work done (W) $=2.3026\text{ RT }\log_{10}\frac{\text{V}_2}{\text{V}_1}$
$=2.3026\times8.3\times400\times\log_{10}\frac{2\text{V}}{\text{V}}$
$=2.3026\times8.3\times400\times0.3010$
$\text{W}=2.30\times10^{3}\text{joule}$ If H is the amount of heat absorbed, then $\text{H}=\frac{\text{W}}{\text{J}}=\frac{2.30\times10^3}{4.2}=548\text{b cal}$
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Question 733 Marks
The efficiency of heat engine cannot be $100\%$. Explain?
Answer
The efficiency of heat engine is given by, $\eta=1-\frac{\text{Q}_2}{\text{Q}_1}$ $\text{Q}_2=$ Heat rejected to the sink, $\text{Q}_1=$ Heat absorbed from the source $\eta=1$ or 100% if and only if $Q_2 = 0$ This cannot happen because if $Q_2 = 0$, then the temperature of the working substance will go on increasing. A stage will come when the temperature of the working substance becomes equal to the temperature of the source. In this situation, there is no transfer of heat from source to the working substance. Hence, we will not get the output.
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Question 743 Marks
Write the expressions for $C_v$ and $C_p$ of a gas in terms of gas constant R and constant $\gamma,$ where $\gamma=\frac{\text{C}_\text{P}}{\text{C}_\nu}$
Answer
We know that $C_P - C_v = R$ and $\frac{\text{C}_\text{P}}{\text{C}_\nu}=\gamma$ From equation (ii) $\text{C}_\text{P}=\gamma\text{C}_\nu$ and sustituting this value in (i), We have $\gamma\text{C}_\nu-\text{C}_\nu=\text{R}$ $\Rightarrow\text{C}_\nu=\frac{\text{R}}{(\gamma+1)}$
$\therefore\text{C}_\text{P}=\gamma.\text{C}_\nu=\frac{\gamma\text{R}}{(\gamma-1)}$
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Question 753 Marks
A person weighing $60 kg$ takes in $2000\ kcal$ diet in a day. If this energy were to be used in heating the person without any loss, what would be his rise in temperature? Given specific heat of human body is $0.83 \mathrm{cal} \mathrm{g}^{-1}{ }^{\circ} \mathrm{C}^{-1}$
Answer
Here, $m = 60kg = 60 \times 10^3g \Delta\text{Q}=2000\text{K cal}=2\times10^6\text{ cal}$ $\Delta\text{Q}=?,\text{C}=0.83\text{cal g}^{-1} {^\circ}\text{C}$ From $\Delta\text{Q}=\text{cm}\Delta\text{T}$ $\Delta\text{T}=\frac{\Delta\text{Q}}{\text{cm}}=\frac{2\times10^6}{0.83\times60\times10^3}$ $=\frac{200}{0.83\times6}=40.16^\circ\text{C}$
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Question 763 Marks
An ideal refrigerator runs between $-23°C$ and $27°C$,
  1. Find the heat rejected to atmosphere for every joule of work input.
  2. Also, find heat extracted from cold body.
  3. Find coefficient of performance of the refrigerator.
Answer
Let heat rejected $Q_1=x$ and $W=1 \mathrm{~J}$ Now, $Q_2=Q_1-W=x-1$ Given, $T_1=273+27=300 \mathrm{~K}, T_2=273-23=250 \mathrm{~K}$
  1. For an ideal process, $\frac{\text{Q}_2}{\text{Q}_1}=\frac{\text{T}_2}{\text{T}_1}$
$\Rightarrow\frac{\text{x}-1}{\text{x}}=\frac{250}{300}$
$\Rightarrow\text{Q}_1=\text{x}=6\text{J}$
  1. $Q_2 = 5J$
  2. Coefficient of performance,
$\beta=\frac{\text{T}_2}{\text{T}_1-\text{T}_2}=\frac{250}{300-250}=5$
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Question 773 Marks
Find the pressure required to compress a gas adiabatically at atmospheric pressure to one fifth of its volume $(\gamma=1.4)$
Answer
Here, $P_1 = 1atm$ Let $V_1 = x c.c.; \text{V}_2=\frac{\text{x}}{5}\text{ c.c.;}$
$\gamma=1.4;\text{ P}=?$ Using the relation, $\text{P}_1\text{V}^\gamma_1=\text{P}_2\text{V}^\gamma_2$
$\therefore\text{P}_2=\text{P}_1\Big(\frac{\text{V}_1}{\text{V}_2}\Big)^\gamma=1\bigg(\frac{\text{x}}{\frac{\text{x}}{5}}\bigg)^{1.4}=(5)^{1.4}$ Taking $\log$ both sides, we get $\log\text{P}_2=1.4\log5$
$=1.4\times0.6990=0.97860$
$\therefore\text{P}_2=9.519\text{ atm}.$
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Question 783 Marks
Differentiate between evaporation and boiling.
Answer
Evaporation is a slow process from the liquid to the gaseous state which takes place at the surface of a liquid and at all temperatures. Boiling is a rapid change of a substance from the liquid to the gaseous state which takes place throughout the mass of the liquid at a definite temperature.
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Question 793 Marks
State Dulong and Petit's law.
Answer
According to the Dulong and Petit's law, the specific heat per mole of a chemically pure crystalline solid is approximately $6 cal mol^{-1}K^{-1}$ or roughly $25J mole^{-1} K^{-1}$. This law is obeyed with quite a good approximation for many substances at the room temperature.
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Question 803 Marks
Establish relation between two specific heats of a gas. Which is greater and why?
Answer
Relation between $C_p$ and $C_v$. Suppose one mole of a gas is heated so that its temperature rises by $d T$. Heat supplied $=1 \times C_p \times d T=C_v d T \ldots$...(i) Since the volume is constant, the gas will not perform external work in accordance with the first law of thermodynamics and the heat supplied will be just equal to the increase in the internal energy of the gas. $\mathrm{dU}=\mathrm{C}_{\mathrm{v}} \mathrm{dT}$...(ii) Let the gas be heated at constant pressure to again increase its temperature by dT , and dQ be the amount of heat supplied, therefore, $\therefore \mathrm{dQ}=1 \times \mathrm{C}_p \times d T=C_p d T$...(iii) The heat supplied at a constant pressure increases the temperature by dT hence, increases its internal energy by dU as well as enables the gas to perform work $d W . d W=P V$...(iv) From the first law of thermodynamics, we have, $d Q=d U+d W$ Substituting the values, we get, $C_p d T=C_v d T+$ PDV But PV $=$ RT (For one mole of the gas) $O r$ PdV $=$ RdT $\therefore C_p d T=C_v d T+R d T$ or $C_p-C_v=R \ldots$ (v) This is the relation between two principal specific heats of the gas when $C_p, C_v$ and $R$ are measured in the units of either heat or of work. $C_p>C_v$ because a part of the energy supplied in the adiabatic process goes to increase the volume of the gas and the remaining increases the temperature.
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Question 813 Marks
Calculate the efficiency of Carnot's engine working between steam point and ice point.
Answer
Here, steam point $\text{T}_1=100^\circ\text{C}$ $=100+273=373\text{K}$ and ice point $\text{T}_2=0^\circ\text{C}$ $=0+273=273\text{K}$ $\therefore\eta=1-\frac{\text{T}_2}{\text{T}_1}$ $=1-\frac{273}{373}=\frac{100}{373}$ $\therefore\eta=\frac{100}{373}\times100\%=26.81\%$
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Question 823 Marks
Prove for an adiabatic process:
  1. $\text{TV}^{\gamma-1}=\text{constant}.$
  2. $\text{P}^{1-\gamma}\text{T}^\gamma=\text{constant.}$
Answer
  1. We know $\text{PV}^{\gamma}=$ constant for adiabatic process.
Also, $\text{PV}=\text{nRT}$
$\therefore\text{P}=\frac{\text{nRT}}{\text{V}}$
Replacing P, we have $\frac{\text{nRT}}{\text{RT}}.\text{V}^{\gamma}=$ constant (or) $\text{TV}^{\gamma-1}=$ constant.
  1. From PV = nRT, we have $\text{V}=\frac{\text{nRT}}{\text{P}}$
Replacing V, we have, $\text{P}\Big(\frac{\text{nRT}}{\text{P}}\Big)^{\gamma}=$ constant.
$\therefore\text{T}^{\gamma}\text{P}^{1-\gamma}=$ constant.
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Question 833 Marks
A refrigerator transfers $250J$ heat per second from $-23^\circ C$ to $25^\circ C$. Find the power consumed, assuming no loss of energy.
Answer
Here, $\mathrm{Q}_2=250 \mathrm{~J} \mathrm{~s}^{-1} \mathrm{~T}_2=-23^{\circ} \mathrm{C}=-23+273=250 \mathrm{~K}_1=25^{\circ} \mathrm{C}=25+273=298 \mathrm{~K}$
We know, $\beta=\frac{\text{Q}_2}{\text{W}}=\frac{\text{T}_2}{\text{T}_1-\text{T}_2}$
$\therefore\text{W}=\frac{\text{Q}_2(\text{T}_1-\text{T}_2)}{\text{T}_2}$
$\text{W}=\frac{250(298-250)}{250}=\frac{250\times48}{250}$
$\text{W}=48\text{J s}^{-1}$
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3 Marks Question - Page 2 - Physics STD 11 Science Questions - Vidyadip