2 marks · definitions
In thermodynamics, a system is a specific portion of the universe that is chosen for study. Everything outside the system is called the surroundings, and the two are separated by a boundary (which can be real or imaginary, fixed or movable).
The classification of these systems depends on whether they can exchange matter and energy (in the forms of heat or work) with their surroundings.
Types of Thermodynamic Systems
1. Open System
An open system can exchange both energy and matter with its surroundings.
Example: A pot of boiling water without a lid. Heat (energy) enters from the stove, and steam (matter) escapes into the air.
2. Closed System
A closed system can exchange energy, but not matter, with its surroundings. The amount of matter inside remains constant.
Example: A sealed cylinder with a piston. Heat can be transferred through the walls, and work can be done by moving the piston, but no gas enters or leaves.
3. Isolated System
An isolated system can exchange neither energy nor matter with its surroundings. It is completely cut off from the rest of the universe.
Example: A perfectly insulated thermos flask (in an ideal sense). In reality, a truly isolated system is difficult to achieve, though the entire Universe is often considered one.
| System Type | Mass Exchange? | Energy Exchange? |
|---|---|---|
| Open | Yes | Yes |
| Closed | No | Yes |
| Isolated | No | No |
Intensive Properties
An intensive property is a physical property of a system that does not depend on the system size or the amount of material present. It is an "intrinsic" characteristic.
Logic: If you have a bucket of water at 25°C and pour it into two smaller cups, the water in each cup is still 25°C.
Example: Temperature. Others include pressure, density, and boiling point.
Extensive Properties
An extensive property is a physical property that does depend on the amount of matter in the system. These properties are additive.
Logic: If you have two identical gold bars, the total mass is the sum of the two. If you take one away, the mass changes.
Example: Mass. Others include volume, total energy, and enthalpy.
Quick Comparison Table
| Property Type | Depends on Amount? | Additive? | Examples |
|---|---|---|---|
| Intensive | No | No | Temperature, Density, Color |
| Extensive | Yes | Yes | Mass, Volume, Heat Capacity |
In thermodynamics, state variables (also known as state functions or state parameters) are physical quantities that describe the current condition or "state" of a system.
Examples: Temperature (T), Pressure (P), Volume (V), Internal Energy (U), Enthalpy (H), Entropy (S), Gibbs Free Energy (G), etc.
Key Characteristics:
- They depend only on the current state of the system, not on how the system reached that state.
- The change in a state variable between two states is independent of the path taken.
- They are exact differentials in mathematical form.
| State Variable | Symbol | Type |
|---|---|---|
| Temperature | T | Intensive |
| Pressure | P | Intensive |
| Volume | V | Extensive |
| Internal Energy | U | Extensive |
| Enthalpy | H | Extensive |
| Entropy | S | Extensive |
Important Note: State variables are different from path variables (like heat and work), which depend on the process taken to reach a state.
A system is in thermodynamic equilibrium when its macroscopic properties (like temperature, pressure, and concentration) remain constant over time and do not change even if the system is left to itself.
For a system to be in true thermodynamic equilibrium, it must simultaneously satisfy three specific conditions:
1. Thermal Equilibrium
There is no flow of heat within the system or between the system and its surroundings. This means the temperature is uniform throughout the entire system.
Condition: ΔT = 0
2. Mechanical Equilibrium
There are no unbalanced forces acting within the system or between the system and its surroundings. The pressure remains constant and uniform at all points.
Condition: ΔP = 0
3. Chemical Equilibrium
The chemical composition of the system remains constant over time. This means no net chemical reactions are occurring, and there is no transfer of matter from one part of the system to another.
Condition: Chemical potential is uniform throughout the system.
| Type of Equilibrium | Condition | Description |
|---|---|---|
| Thermal | ΔT = 0 | Uniform temperature, no heat flow |
| Mechanical | ΔP = 0 | Uniform pressure, no unbalanced forces |
| Chemical | μ = constant | Uniform chemical potential, no composition change |
Important Note: All three conditions must be satisfied simultaneously for a system to be in complete thermodynamic equilibrium. If any one condition is not met, the system is not in true thermodynamic equilibrium.
An isothermal process is a thermodynamic process in which the temperature of the system remains constant throughout the process (\(\Delta T = 0\)).
Note:
(1) Work done in isothermal process (for ideal gas):
\(W = nRT \ln \left( \frac{V_2}{V_1} \right) = 2.303 \, nRT \log_{10} \left( \frac{V_2}{V_1} \right)\)
(2) PV diagram: In an isothermal process, the curve is a rectangular hyperbola (\(PV = \text{constant}\)).
An adiabatic process is a thermodynamic process in which no heat exchange takes place between the system and its surroundings (\(Q = 0\)).
Special Notes:
(1) For an ideal gas, adiabatic process follows:
\(PV^\gamma = \text{constant}\)
\(TV^{\gamma-1} = \text{constant}\)
\(T^\gamma P^{1-\gamma} = \text{constant}\)
where \(\gamma = \frac{C_p}{C_v}\) (ratio of specific heats).
(2) Work done in adiabatic process (for ideal gas):
\(W = \frac{P_1V_1 - P_2V_2}{\gamma - 1} = \frac{nR(T_1 - T_2)}{\gamma - 1}\)
Examples:
- Rapid compression in a diesel engine (causes ignition)
- Expansion of gas in a nozzle
- Sound wave propagation in air
- Cloud formation due to rising air expansion
1. Isobaric Process
An isobaric process is a thermodynamic process in which the pressure (\(P\)) of the system remains constant throughout the change (\(\Delta P = 0\)).
2. Isochoric Process
An isochoric process (also known as an isometric or isovolumetric process) is a thermodynamic process in which the volume (\(V\)) of the system remains constant (\(\Delta V = 0\)).
| Process | Constant Variable | Work Done (W) |
|---|---|---|
| Isobaric | Pressure (\(P\)) | \(P\Delta V\) |
| Isochoric | Volume (\(V\)) | Zero (\(0\)) |
| Aspect | Heat | Temperature |
|---|---|---|
| Definition | Heat is the total energy of molecular motion in a substance. | Temperature is the measure of the average kinetic energy of molecules. |
| Symbol | \(Q\) | \(T\) |
| Unit (SI) | Joule (J) | Kelvin (K) or °C |
| Property Type | Extensive property (depends on amount of substance) | Intensive property (independent of amount) |
| Flow | Heat flows from hotter to colder body | Temperature determines direction of heat flow |
| Measurement | Measured by calorimeter | Measured by thermometer |
| Effect | Heat can change temperature, state, or do work | Temperature indicates degree of hotness or coldness |
Example: A cup of coffee at 80°C has higher temperature than a swimming pool at 30°C, but the swimming pool contains more heat (more total thermal energy) due to its larger mass.
Internal energy (U) is the total energy stored within a system at the molecular level. It is the sum of the microscopic kinetic energies and potential energies of all the atoms or molecules that make up the system.
Note:
- It is an extensive property (depends on amount of substance)
- It is a state function (depends only on initial and final states)
- For an ideal gas, internal energy depends only on temperature
- Change in internal energy: \(\Delta U = Q - W\) (First Law of Thermodynamics)
In a cyclic process, a system starts at an initial state, undergoes a series of changes, and eventually returns to its original state. Because the system returns to its starting point, the net change in internal energy (ΔU = 0).
From the First Law of Thermodynamics:
$$\Delta U = Q - W$$
Since ΔU = 0, we get:
$$Q = W$$
Therefore, in a cyclic process:
- The net work done by the system equals the net heat absorbed by the system.
- On a PV diagram, the work done is represented by the area enclosed by the cycle.
$$\text{Work} = \oint P \, dV = \text{Area enclosed in PV diagram}$$
In a P−V diagram (Pressure-Volume diagram), the area under the curve represents the total work done by or on the system during a thermodynamic process.
$$\text{Work} = \int_{V_i}^{V_f} P \, dV$$
The area under the curve equals the magnitude of work. The sign depends on the direction:
- Expansion (volume increases) → Work done by the system (positive)
- Compression (volume decreases) → Work done on the system (negative)
It states that energy can neither be created nor destroyed; it can only be converted from one form to another or transferred between a system and its surroundings.
Mathematical Expression
The law is expressed by the following equation:
$$\Delta Q = \Delta U + W$$
Where:
- ΔQ: The net heat added to the system.
- ΔU: The change in the internal energy of the system.
- W: The work done by the system on its surroundings.
Sign Conventions
To use the formula correctly, it is vital to follow these standard sign conventions:
| Quantity | Positive (+) | Negative (-) |
|---|---|---|
| Heat (Q) | Heat is absorbed by the system | Heat is released by the system |
| Work (W) | Work is done by the system (Expansion) | Work is done on the system (Compression) |
| Internal Energy (U) | Temperature increases | Temperature decreases |
Specific heat at constant volume (Cv) is defined as the amount of heat required to raise the temperature of a unit mass (or one mole) of a substance by one degree Celsius (or one Kelvin) while the volume of the system is kept constant.
Mathematically,
\(C_v = \frac{1}{n} \left( \frac{dQ}{dT} \right)_V\)
Where:
- \(n\) = number of moles (for molar specific heat)
- \(dQ\) = heat supplied
- \(dT\) = change in temperature
- \(V\) = constant volume
Note:
For an ideal gas:
\(C_v = \frac{f}{2}R\)
where \(f\) = degrees of freedom and \(R\) = universal gas constant.
Relation with internal energy:
\(dU = nC_v dT\)
At constant volume, all heat supplied goes into increasing internal energy (no work done).
Specific heat at constant pressure (Cp) is defined as the amount of heat required to raise the temperature of a unit mass (or one mole) of a substance by one degree Celsius (or one Kelvin) while the pressure of the system is kept constant.
Mathematically,
\(C_p = \frac{1}{n} \left( \frac{dQ}{dT} \right)_P\)
Where:
- \(n\) = number of moles (for molar specific heat)
- \(dQ\) = heat supplied
- \(dT\) = change in temperature
- \(P\) = constant pressure
Note:
For an ideal gas:
\(C_p = C_v + R\)
\(C_p = \left( \frac{f}{2} + 1 \right) R\)
where \(f\) = degrees of freedom and \(R\) = universal gas constant.
Relation with enthalpy:
\(dH = nC_p dT\)
At constant pressure, heat supplied equals increase in enthalpy.
Ratio of specific heats:
\(\gamma = \frac{C_p}{C_v}\)
For an ideal gas, the difference between molar specific heat at constant pressure (\(C_p\)) and molar specific heat at constant volume (\(C_v\)) is given by:
\(C_p - C_v = R\)
where \(R\) is the universal gas constant (\(R = 8.314 \, \text{J mol}^{-1} \text{K}^{-1}\)).
This relation is known as Mayer's formula.
A heat engine is a device that converts heat energy into mechanical work by operating in a cyclic process. It absorbs heat from a high-temperature source (reservoir), converts a part of it into useful work, and rejects the remaining heat to a low-temperature sink.
Note:
Efficiency of a heat engine:
\(\eta = \frac{W}{Q_H} = 1 - \frac{Q_L}{Q_H}\)
Examples of heat engines: Steam engines, internal combustion engines (petrol/diesel engines), gas turbines, etc.
The efficiency (η) of a heat engine is defined as the ratio of the net work done (W) by the engine to the total heat absorbed (QH) from the high-temperature source.
General Formula
For any heat engine, the efficiency is given by:
$$\eta = \frac{W}{Q_H}$$
Since \(W = Q_H - Q_L\) (where QL is the heat rejected to the sink), the formula can also be written as:
$$\eta = 1 - \frac{Q_L}{Q_H}$$
A refrigerator is a device that transfers heat from a low-temperature reservoir (cold body) to a high-temperature reservoir (hot body) by doing external work on the system. It operates on the reverse cycle of a heat engine.
Note:
Coefficient of Performance (COP) of a refrigerator:
\(COP = \frac{Q_L}{W} = \frac{Q_L}{Q_H - Q_L}\)
For a reversible (Carnot) refrigerator: \(COP = \frac{T_L}{T_H - T_L}\)
A Carnot engine is a theoretical, idealized heat engine that operates on the Carnot cycle. It is a perfectly reversible engine that provides the maximum possible efficiency that any engine can achieve when operating between two specific temperatures.
Note:
Carnot Efficiency (η)
\(η = 1 - \frac{T₂}{T₁}\)
where T₁ = Temperature of source (hot reservoir)
T₂ = Temperature of sink (cold reservoir)
(Temperatures in Kelvin)
3 marks · conceptual
For an ideal gas, enthalpy \(H = U + PV = U + nRT\)
Differentiating with respect to temperature at constant pressure:
\(\left( \frac{dH}{dT} \right)_P = \left( \frac{dU}{dT} \right)_P + nR\)
Since for ideal gas, internal energy depends only on temperature, \(\left( \frac{dU}{dT} \right)_P = \left( \frac{dU}{dT} \right)_V = nC_v\)
And \(\left( \frac{dH}{dT} \right)_P = nC_p\)
Therefore, \(nC_p = nC_v + nR\)
\(\therefore C_p - C_v = R\)
No, internal energy is NOT path dependent. It is a state function.
Justification:
- Definition: Internal energy (\(U\)) depends only on the current state of the system (temperature, pressure, volume, composition), not on how the system reached that state.
- Mathematical proof: The change in internal energy \(\Delta U\) between two states is given by:
\(\Delta U = U_{\text{final}} - U_{\text{initial}}\)
It depends only on the initial and final states, regardless of the path taken.
- First Law of Thermodynamics: \(\Delta U = Q - W\). While \(Q\) (heat) and \(W\) (work) are path-dependent, their difference \(\Delta U\) is path-independent.
- Cyclic process: In a cyclic process, the system returns to its initial state. For any cycle:
\(\oint dU = 0\)
This means the net change in internal energy around any closed path is zero, proving it's a state function.
- For ideal gas: Internal energy depends only on temperature (\(U = \frac{f}{2}nRT\)). No matter what path you take, if initial and final temperatures are same, \(\Delta U = 0\).
3 marks · derivations
Work done in Isothermal Process:
We know,
\(W = \int_{V_1}^{V_2} P \, dV\)
For an ideal gas,
\(PV = nRT\)
\(\implies P = \frac{nRT}{V}\)
Substituting the value of \(P\) in the work equation:
\(W = \int_{V_1}^{V_2} \frac{nRT}{V} \, dV\)
Since \(n, R, T\) are constants:
\(W = nRT \int_{V_1}^{V_2} \frac{1}{V} \, dV\)
Integrating \(\frac{1}{V}\) with respect to \(V\):
\(W = nRT [\ln V]_{V_1}^{V_2}\)
\(W = nRT (\ln V_2 - \ln V_1)\)
\(W = nRT \ln \left( \frac{V_2}{V_1} \right)\)
Converting to \(\log_{10}\):
\(W = 2.303 \, nRT \log_{10} \left( \frac{V_2}{V_1} \right)\)
Work done in Adiabatic Process:
For an adiabatic process:
\(PV^\gamma = K \text{ (constant)}\)
\(\implies P = \frac{K}{V^\gamma}\)
Total work done:
\(W = \int_{V_1}^{V_2} P \, dV\)
Substituting the value of \(P\):
\(W = \int_{V_1}^{V_2} \frac{K}{V^\gamma} \, dV\)
\(W = K \int_{V_1}^{V_2} V^{-\gamma} \, dV\)
Integrating \(V^{-\gamma}\) with respect to \(V\):
\(W = K \left[ \frac{V^{-\gamma+1}}{-\gamma+1} \right]_{V_1}^{V_2}\)
\(W = \frac{K}{1-\gamma} [V_2^{1-\gamma} - V_1^{1-\gamma}]\)
\(W = \frac{1}{1-\gamma} [KV_2^{1-\gamma} - KV_1^{1-\gamma}]\)
Since \(P_1V_1^\gamma = P_2V_2^\gamma = K\), we can substitute \(K\) accordingly:
\(W = \frac{1}{1-\gamma} [(P_2V_2^\gamma)V_2^{1-\gamma} - (P_1V_1^\gamma)V_1^{1-\gamma}]\)
\(W = \frac{1}{1-\gamma} [P_2V_2 - P_1V_1]\)
Using Ideal Gas Equation (\(PV = nRT\)):
\(P_1V_1 = nRT_1 \text{ and } P_2V_2 = nRT_2\)
Substituting these values:
\(W = \frac{1}{1-\gamma} [nRT_2 - nRT_1]\)
\(W = \frac{nR}{1-\gamma} (T_2 - T_1)\)
Rearranging for \((\gamma - 1)\):
\(W = \frac{nR}{\gamma - 1} (T_1 - T_2)\)



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