JEE Physics Thermodynamics Notes Set 01

Official JEE Physics Revision Material: JEE Physics Thermodynamics Notes Set 01

Explore reliable concept summaries and revision materials through the JEE Physics Thermodynamics Notes Set 01. Tailored for JEE learners, utilizing these notes for Physics Thermodynamics ensures thorough preparation and strengthens core academic definitions before final evaluations.

Chapter-wise Concept Summaries: Thermodynamics

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Basic Terms

 

A system is the part of the universe under study and everything else is the surroundings. State variables such as pressure P, volume V, temperature T and internal energy U describe the state. They are state functions: their change depends only on the initial and final states. Heat Q and work W depend on the path followed.
The zeroth law says that two bodies each in thermal equilibrium with a third body are in equilibrium with each other, which is the basis of temperature measurement. The internal energy of an ideal gas depends only on temperature: \( U = \dfrac{f}{2}nRT \) and \( \Delta U = nC_V\Delta T \) in every process.

 

Work and the First Law

 

When a gas changes its volume the work done by it is \( W = \int P\,dV \), the area under the P-V curve. W is positive in expansion and negative in compression. In a closed loop the net work equals the area enclosed: positive for a clockwise loop and negative for an anticlockwise one.
First law: \( Q = \Delta U + W \). Heat supplied to a system goes partly into raising its internal energy and partly into the work it does. It is the law of conservation of energy. Sign convention used here: Q is positive when heat enters the system and W is positive when the system does work.

 

Thermodynamic Processes

 

ProcessConditionWork done by gasHeat Q\( \Delta U \)
IsochoricV constant0\( nC_V\Delta T \)\( nC_V\Delta T \)
IsobaricP constant\( P\Delta V = nR\Delta T \)\( nC_P\Delta T \)\( nC_V\Delta T \)
IsothermalT constant, PV = const\( nRT\ln\dfrac{V_2}{V_1} \)equals W0
AdiabaticQ = 0, \( PV^\gamma \) = const\( \dfrac{P_1V_1 - P_2V_2}{\gamma - 1} = \dfrac{nR(T_1-T_2)}{\gamma-1} \)0\( -W \)

 

Adiabatic relations: \( PV^\gamma = \text{constant} \), \( TV^{\gamma-1} = \text{constant} \) and \( P^{1-\gamma}T^\gamma = \text{constant} \). On a P-V diagram the adiabatic curve is steeper than the isothermal curve through the same point, with slope \( \gamma \) times larger. The bulk modulus of a gas is P for an isothermal change and \( \gamma P \) for an adiabatic change. In a polytropic process \( PV^n = \text{constant} \) the molar heat capacity is \( C = C_V + \dfrac{R}{1-n} \).
In free expansion into a vacuum no work is done and, if the container is insulated, \( Q = 0 \) and \( \Delta U = 0 \): an ideal gas keeps its temperature. Sudden compression or expansion is nearly adiabatic, so a pumped tyre warms up and a gas that escapes quickly from a bottle cools.

 

Specific Heats of Gases

 

Because a gas expands when heated at constant pressure, \( C_P > C_V \). Mayer's relation: \( C_P - C_V = R \). With f degrees of freedom \( C_V = \dfrac{f}{2}R \) and \( \gamma = \dfrac{C_P}{C_V} = 1 + \dfrac{2}{f} \). At constant pressure the fractions of the heat used are \( \dfrac{\Delta U}{Q} = \dfrac{1}{\gamma} \) and \( \dfrac{W}{Q} = 1 - \dfrac{1}{\gamma} \): 60 % and 40 % for a monatomic gas, 71 % and 29 % for a diatomic gas. The specific heat is zero in an adiabatic process and infinite in an isothermal one.

 

Second Law, Heat Engines and Refrigerators

 

Kelvin-Planck statement: no cyclic engine can take heat from a single reservoir and convert all of it into work. Clausius statement: heat cannot flow by itself from a colder body to a hotter body. Both statements are equivalent and they set the direction of natural processes. Real processes are irreversible because of friction and other dissipative effects.
A heat engine takes \( Q_1 \) from a hot source, does work \( W = Q_1 - Q_2 \) and rejects \( Q_2 \) to a sink. Its efficiency is \( \eta = \dfrac{W}{Q_1} = 1 - \dfrac{Q_2}{Q_1} \). A refrigerator works in reverse, with coefficient of performance \( \beta = \dfrac{Q_2}{W} = \dfrac{Q_2}{Q_1 - Q_2} \).
The Carnot engine uses two isothermal and two adiabatic steps, is reversible, and has the greatest possible efficiency between two temperatures: \[ \eta = 1 - \dfrac{T_2}{T_1}, \qquad \beta = \dfrac{T_2}{T_1 - T_2}. \] No engine working between the same two reservoirs can be more efficient. The efficiency is raised by raising the source temperature or lowering the sink temperature; it is always below 100 % because the sink cannot be at absolute zero.

 

Worked Examples

 

Example 1. A gas absorbs 400 J of heat and does 150 J of work. Find the change in its internal energy. If it is then compressed isothermally, with 200 J of work done on it, how much heat flows out?
Answer:
\( \Delta U = Q - W = 400 - 150 = \) 250 J.
In an isothermal process \( \Delta U = 0 \), so \( Q = W = -200 \) J: 200 J of heat is released.

 

Example 2. A monatomic ideal gas at 300 K is compressed adiabatically to 1/8 of its volume. Find the final temperature.
Answer:
\( \gamma = \dfrac{5}{3} \) and \( TV^{\gamma-1} = \text{constant} \).
\( T_2 = 300\times8^{2/3} = 300\times4 = \) 1200 K.

 

Example 3. 2 mol of a diatomic gas is heated at constant pressure from 300 K to 400 K. Find Q, W and \( \Delta U \) (R = 8.31 J/mol K).
Answer:
\( Q = nC_P\Delta T = 2\times\dfrac{7}{2}\times8.31\times100 = \) 5817 J.
\( W = nR\Delta T = 2\times8.31\times100 = \) 1662 J.
\( \Delta U = Q - W = \) 4155 J.

 

Example 4. A Carnot engine works between 527°C and 127°C and takes 2000 J of heat per cycle from the source. Find its efficiency, the work per cycle and the heat rejected.
Answer:
\( T_1 = 800 \) K, \( T_2 = 400 \) K, so \( \eta = 1 - \dfrac{400}{800} = \) 50 %.
\( W = 0.5\times2000 = \) 1000 J; \( Q_2 = 2000 - 1000 = \) 1000 J.

Study Material and Revision Notes for JEE Physics Thermodynamics

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