Materials
Compressed notes for fast review.
Waves and Oscillations
Definition
A wave is a disturbance that travels through space and time, transferring energy without transferring matter. Oscillation is the repetitive variation, typically in time, of some measure about a central value.
Key Properties
- Wavelength (λ): Distance between two consecutive identical points
- Frequency (f): Number of oscillations per unit time
- Period (T): Time for one complete oscillation
- Wave speed (v): Speed at which the wave propagates
Important Formulas
v = fλ
T = 1/f
ω = 2πf = 2π/TExample Problem
Problem: A wave has a frequency of 50 Hz and wavelength of 0.2 m. Find the wave speed.
Solution:
Given: f = 50 Hz, λ = 0.2 m
Using: v = fλ
v = 50 × 0.2 = 10 m/sPeriodic Motion
Definition
Periodic motion is motion that repeats itself at regular intervals of time. The motion returns to the same state after a fixed time period.
Key Characteristics
- Particular Point: The motion passes through the same position repeatedly
- Particular Time Interval: The motion repeats after a fixed time period (T)
- Same Direction: At corresponding points in different cycles, velocity has the same direction
Mathematical Description
For periodic motion: x(t + T) = x(t) for all t
Example
- Simple pendulum swinging back and forth
- Mass on a spring oscillating up and down
- Earth's rotation around the sun
Simple Harmonic Motion
Definition
Simple Harmonic Motion (SHM) is a type of periodic motion where the restoring force is directly proportional to the displacement from equilibrium position and acts in the opposite direction.
Mathematical Form
F = -kx
a = -ω²xWhere:
- F = restoring force
- k = force constant
- x = displacement
- ω = angular frequency
General Solution
x(t) = A cos(ωt + φ)Where:
- A = amplitude
- ω = angular frequency
- φ = phase constant
Example Problem
Problem: A mass of 2 kg is attached to a spring with k = 50 N/m. Find the period and frequency of oscillation.
Solution:
Given: m = 2 kg, k = 50 N/m
ω = √(k/m) = √(50/2) = √25 = 5 rad/s
T = 2π/ω = 2π/5 = 1.26 s
f = 1/T = 5/(2π) = 0.796 HzAngular Velocity & Frequency
Definition
Angular velocity (ω) is the rate of change of angular displacement with respect to time. In Simple Harmonic Motion (SHM), it represents how fast the oscillator would move if it were moving in a circle with the same period.
Frequency (f) is the number of complete oscillations per unit time.
Mathematical Relationships
ω = 2πf = 2π/T
f = 1/T = ω/(2π)
T = 2π/ω = 1/fWhere:
- ω = angular velocity (rad/s)
- f = frequency (Hz or s⁻¹)
- T = period (s)
Physical Significance
- Angular velocity connects linear Simple Harmonic Motion (SHM) to circular motion
- Higher frequency means faster oscillations
- Angular velocity determines the rate of phase change in Simple Harmonic Motion (SHM)
For Different Systems
Spring-Mass System:
ω = √(k/m)
f = (1/2π)√(k/m)Simple Pendulum:
ω = √(g/L)
f = (1/2π)√(g/L)Physical Pendulum:
ω = √(mgd/I)
f = (1/2π)√(mgd/I)Example Problem
Problem: A mass-spring system has a spring constant k = 100 N/m and mass m = 4 kg. Find the angular velocity, frequency, and period.
Solution:
Given: k = 100 N/m, m = 4 kg
Angular velocity:
ω = √(k/m) = √(100/4) = √25 = 5 rad/s
Frequency:
f = ω/(2π) = 5/(2π) = 0.796 Hz
Period:
T = 1/f = 2π/ω = 2π/5 = 1.26 sUnits and Conversions
- Angular velocity: rad/s (radians per second)
- Frequency: Hz = s⁻¹ = cycles per second
- Period: s (seconds)
Conversion:
- 1 revolution = 2π radians
- 1 Hz = 2π rad/s of angular velocity
Velocity & Acceleration in Simple Harmonic Motion (SHM)
Velocity
If position: x(t) = A cos(ωt + φ)
Then velocity: v(t) = dx/dt = -Aω sin(ωt + φ)
Maximum velocity: v_max = Aω (at equilibrium position)
Acceleration
Acceleration: a(t) = dv/dt = -Aω² cos(ωt + φ) = -ω²x(t)
Maximum acceleration: a_max = Aω² (at extreme positions)
Key Relationships
v² = ω²(A² - x²)
a = -ω²xExample Problem
Problem: A particle in Simple Harmonic Motion (SHM) has amplitude 0.1 m and angular frequency 5 rad/s. Find velocity and acceleration when x = 0.06 m.
Solution:
Given: A = 0.1 m, ω = 5 rad/s, x = 0.06 m
Velocity:
v² = ω²(A² - x²)
v² = 25(0.01 - 0.0036) = 25(0.0064) = 0.16
v = ±0.4 m/s
Acceleration:
a = -ω²x = -25 × 0.06 = -1.5 m/s²Springs in Simple Harmonic Motion (SHM)
Definition
Springs in Simple Harmonic Motion refer to elastic systems where a mass attached to a spring oscillates about its equilibrium position under the restoring force provided by the spring.
Hooke's Law
F = -kxSpring-Mass System
For a mass m attached to a spring with spring constant k:
ω = √(k/m)
T = 2π√(m/k)
f = (1/2π)√(k/m)Energy Considerations
Total Energy = (1/2)kA²
Kinetic Energy = (1/2)mv²
Potential Energy = (1/2)kx²Example Problem
Problem: A 0.5 kg mass on a spring oscillates with period 2 s. Find the spring constant.
Solution:
Given: m = 0.5 kg, T = 2 s
T = 2π√(m/k)
2 = 2π√(0.5/k)
1/π = √(0.5/k)
1/π² = 0.5/k
k = 0.5π² = 4.93 N/mDisplacement
Definition
Displacement in Simple Harmonic Motion (SHM) is the distance from the equilibrium position, measured along the line of motion.
Mathematical Expression
x(t) = A cos(ωt + φ)Key Points
- Displacement varies sinusoidally with time
- Maximum displacement = Amplitude (A)
- At equilibrium: x = 0
- At extremes: x = ±A
Phase Relationships
Important phase differences in Simple Harmonic Motion (SHM):
| Position | Displacement (x) | Velocity (v) | Acceleration (a) |
|---|---|---|---|
| Extreme position | Maximum (±A) | Zero | Maximum (opposite to x) |
| Equilibrium | Zero | Maximum | Zero |
| Intermediate | Between 0 and A | Between 0 and max | Between 0 and max |
Phase differences:
- Velocity leads displacement by π/2 (90°)
- Acceleration leads velocity by π/2 (90°)
- Acceleration opposes displacement (π or 180° out of phase)
Mathematical relationships:
x(t) = A cos(ωt + φ) [displacement]
v(t) = -Aω sin(ωt + φ) [velocity leads x by π/2]
a(t) = -Aω² cos(ωt + φ) [acceleration opposes x]Energy in Simple Harmonic Motion (SHM)
Total Mechanical Energy
E = (1/2)kA² = constantEnergy Distribution
At any instant:
E = KE + PE = (1/2)mv² + (1/2)kx²Energy Variations
- At equilibrium (x = 0): KE = maximum, PE = 0
- At extremes (x = ±A): KE = 0, PE = maximum
- At intermediate positions: Both KE and PE are non-zero
Example Problem
Problem: A mass oscillates with amplitude 0.05 m on a spring (k = 100 N/m). Find total energy and kinetic energy when x = 0.03 m.
Solution:
Given: A = 0.05 m, k = 100 N/m, x = 0.03 m
Total Energy:
E = (1/2)kA² = (1/2) × 100 × (0.05)² = 0.125 J
Potential Energy at x = 0.03 m:
PE = (1/2)kx² = (1/2) × 100 × (0.03)² = 0.045 J
Kinetic Energy:
KE = E - PE = 0.125 - 0.045 = 0.08 JAmplitude
Definition
Amplitude (A) is the maximum displacement from the equilibrium position in Simple Harmonic Motion (SHM).
Characteristics
- Always positive
- Determines the energy of the system:
E = (1/2)kA² - Determines maximum velocity:
v_max = Aω - Determines maximum acceleration:
a_max = Aω²
Determining Amplitude
From initial conditions:
A = √(x₀² + (v₀/ω)²)Where x₀ and v₀ are initial position and velocity.
Kinetic Energy
Definition
Kinetic Energy is the energy due to motion of the oscillating particle.
Formula
KE = (1/2)mv²In Simple Harmonic Motion (SHM):
KE = (1/2)m[Aω sin(ωt + φ)]²
KE = (1/2)mA²ω² sin²(ωt + φ)Alternative Form
KE = (1/2)ω²(A² - x²) × m
KE = (1/2)k(A² - x²)Maximum KE
KE_max = (1/2)mA²ω² = (1/2)kA²This occurs at equilibrium position (x = 0).
Potential Energy
Definition
Potential Energy is the energy stored due to displacement from equilibrium.
Formula
PE = (1/2)kx²Characteristics
- Zero at equilibrium position
- Maximum at extreme positions:
PE_max = (1/2)kA² - Varies as square of displacement
Graph
PE vs displacement is a parabola with vertex at origin.
Simple Pendulum
Definition
A simple pendulum consists of a point mass suspended by a massless, inextensible string from a fixed point.
Small Angle Approximation
For small angles (θ < 15°): sin θ ≈ θ
Period Formula
T = 2π√(L/g)Where:
- L = length of pendulum
- g = acceleration due to gravity
Key Points
- Period is independent of mass and amplitude (for small angles)
- Period depends only on length and gravitational acceleration
Example Problem
Problem: A simple pendulum has length 1 m. Find its period on Earth (g = 9.8 m/s²).
Solution:
Given: L = 1 m, g = 9.8 m/s²
T = 2π√(L/g) = 2π√(1/9.8) = 2π√(0.102) = 2π × 0.319 = 2.01 sPendulum in a Lift
Effective Gravity
When a pendulum is in a lift, the effective gravity changes:
Lift at rest or constant velocity: g_eff = g
Lift accelerating upward: g_eff = g + a
Lift accelerating downward: g_eff = g - a
Free falling lift: g_eff = 0 (pendulum doesn't oscillate)
Modified Period
T = 2π√(L/g_eff)Example Problem
Problem: A pendulum has period 2 s when lift is at rest. Find period when lift accelerates upward at 2 m/s².
Solution:
Given: T₀ = 2 s, a = 2 m/s² (upward)
At rest: T₀ = 2π√(L/g) = 2 s
Therefore: L/g = 1/π²
In accelerating lift:
g_eff = g + a = 9.8 + 2 = 11.8 m/s²
T = 2π√(L/g_eff) = 2π√(L/11.8)
T = 2π√((1/π²) × (9.8/11.8)) = 2√(9.8/11.8) = 1.82 sCenter of Mass (Control of Mass)
Definition
The center of mass (also referred to as "control of mass" in some contexts) is the point where the total mass of a system can be considered to be concentrated for the purpose of analyzing translational motion. It's the average position of all mass elements in a system.
For Discrete Masses
x_cm = (m₁x₁ + m₂x₂ + ... + mₙxₙ)/(m₁ + m₂ + ... + mₙ)For Continuous Mass Distribution
x_cm = (1/M) ∫ x dmProperties
- Center of mass moves as if all external forces act on it
- Internal forces don't affect center of mass motion
- For symmetric objects, center of mass is at geometric center
Example Problem
Problem: Two masses m₁ = 3 kg at x₁ = 2 m and m₂ = 2 kg at x₂ = 8 m. Find center of mass.
Solution:
x_cm = (m₁x₁ + m₂x₂)/(m₁ + m₂)
x_cm = (3×2 + 2×8)/(3+2) = (6+16)/5 = 4.4 mTorque and Moment of Inertia
Torque
Torque (τ) is the rotational equivalent of force.
τ = r × F = rF sin θ
τ = IαWhere:
- r = distance from axis of rotation
- F = applied force
- θ = angle between r and F
- I = moment of inertia
- α = angular acceleration
Moment of Inertia
Moment of inertia (I) is the rotational equivalent of mass.
For point masses:
I = Σ mᵢrᵢ²For continuous distributions:
I = ∫ r² dmCommon Moments of Inertia
- Solid sphere about center:
I = (2/5)MR² - Solid cylinder about axis:
I = (1/2)MR² - Rod about center:
I = (1/12)ML² - Rod about end:
I = (1/3)ML²
Example Problem
Problem: A solid cylinder (M = 5 kg, R = 0.2 m) rotates about its axis. Find moment of inertia.
Solution:
For solid cylinder about its axis:
I = (1/2)MR² = (1/2) × 5 × (0.2)² = 0.1 kg⋅m²Linear vs Circular Motion
Linear Motion - Force Changes Inertia
In linear motion:
- Newton's 2nd Law:
F = ma - Inertia: Resistance to change in linear motion (mass)
- Force: Causes acceleration (change in velocity)
Circular Motion - Torque Changes Inertia
In rotational motion:
- Rotational 2nd Law:
τ = Iα - Rotational Inertia: Resistance to change in rotational motion (moment of inertia)
- Torque: Causes angular acceleration (change in angular velocity)
Analogies
| Linear Motion | Rotational Motion |
|---|---|
| Force (F) | Torque (τ) |
| Mass (m) | Moment of Inertia (I) |
| Acceleration (a) | Angular Acceleration (α) |
| Velocity (v) | Angular Velocity (ω) |
| Displacement (x) | Angular Displacement (θ) |
Physical Pendulum
Definition
A physical pendulum is any rigid body that oscillates under gravity about a horizontal axis that doesn't pass through its center of mass.
Period Formula
T = 2π√(I/mgd)Where:
- I = moment of inertia about the pivot point
- m = mass of the body
- g = acceleration due to gravity
- d = distance from pivot to center of mass
Parallel Axis Theorem
I = I_cm + md²Where I_cm is the moment of inertia about center of mass.
Example Problem
Problem: A uniform rod of length L = 1 m and mass m = 2 kg oscillates about one end. Find the period.
Solution:
For rod about end: I = (1/3)mL²
Distance to center of mass: d = L/2
T = 2π√(I/mgd) = 2π√((1/3)mL²/(mg×L/2))
T = 2π√((1/3)L²/(g×L/2)) = 2π√(2L/3g)
T = 2π√(2×1/(3×9.8)) = 2π√(0.068) = 1.64 sThermodynamics
Definition
Thermodynamics is the branch of physics that deals with heat, work, and temperature, and their relation to energy, radiation, and physical properties of matter.
Laws of Thermodynamics
The fundamental laws governing energy transfer and transformation in thermodynamic systems are covered in detail in the First Law of Thermodynamics (Enhanced) section below.
Key Concepts
- System: The part of universe under study
- Surroundings: Everything else
- State variables: P, V, T, U, S
- Process: Path between two states
Types of Systems
- Open: Mass and energy can cross boundary
- Closed: Only energy can cross boundary
- Isolated: Neither mass nor energy can cross boundary
Ideal Gas Laws
Individual Gas Laws:
- Boyle's Law (constant T):
PV = constant - Charles's Law (constant P):
V/T = constant - Gay-Lussac's Law (constant V):
P/T = constant
Combined Gas Law:
(P₁V₁)/T₁ = (P₂V₂)/T₂Ideal Gas Equation:
PV = nRTWhere R = 8.314 J/(mol·K) = universal gas constant
Isothermal Process
Definition
An isothermal process is one where temperature remains constant throughout.
Characteristics
ΔT = 0ΔU = 0(for ideal gas)Q = W(all heat goes into work)
Ideal Gas Law
PV = constant
P₁V₁ = P₂V₂Work Done
W = nRT ln(V₂/V₁) = nRT ln(P₁/P₂)Example Problem
Problem: 2 moles of ideal gas at 300 K expand isothermally from 10 L to 20 L. Find work done.
Solution:
Given: n = 2 mol, T = 300 K, V₁ = 10 L, V₂ = 20 L
R = 8.314 J/(mol⋅K)
W = nRT ln(V₂/V₁)
W = 2 × 8.314 × 300 × ln(20/10)
W = 4988.4 × ln(2) = 4988.4 × 0.693 = 3458 JAdiabatic Process
Definition
An adiabatic process is one where no heat is exchanged with surroundings (Q = 0).
Characteristics
Q = 0ΔU = -W- Temperature changes during process
Adiabatic Relations
PVᵞ = constant
TVᵞ⁻¹ = constant
TPᵞ⁻¹/ᵞ = constantWhere γ = Cp/Cv (adiabatic index)
Work Done
W = (P₁V₁ - P₂V₂)/(γ - 1)Example Problem
Problem: An ideal gas (γ = 1.4) expands adiabatically from P₁ = 5 atm, V₁ = 2 L to V₂ = 8 L. Find final pressure.
Solution:
Given: γ = 1.4, P₁ = 5 atm, V₁ = 2 L, V₂ = 8 L
Using PVᵞ = constant:
P₁V₁ᵞ = P₂V₂ᵞ
P₂ = P₁(V₁/V₂)ᵞ = 5 × (2/8)^1.4 = 5 × (0.25)^1.4 = 5 × 0.0946 = 0.473 atmReversible Process
Definition
A reversible process is an ideal thermodynamic process that can be reversed without leaving any trace on the surroundings. It proceeds infinitely slowly through a series of equilibrium states.
Characteristics
- Quasi-static: Proceeds very slowly
- No friction: No energy lost to friction
- No heat conduction: No spontaneous heat transfer
- Pressure equilibrium: System pressure always equals external pressure
Examples
- Slow compression/expansion of gas in a frictionless piston
- Carnot cycle (theoretical)
- Slow charging/discharging of a battery
Key Points
- Maximum work output for expansion
- Minimum work input for compression
- Entropy of universe remains constant
- Real processes are always irreversible
Mathematical Condition
For a reversible process:
dS_universe = dS_system + dS_surroundings = 0Efficiency
Definition
Efficiency is the ratio of useful work output to the total energy input in any process or machine.
General Formula
η = Work Done (Output) / Energy Input × 100%
η = W_out / Q_in × 100%For Heat Engines
η = (Q_H - Q_C) / Q_H = 1 - Q_C/Q_H
η = W / Q_HWhere:
- Q_H = heat absorbed from hot reservoir
- Q_C = heat rejected to cold reservoir
- W = net work done
Maximum Efficiency (Carnot)
η_max = 1 - T_C/T_HExample Problem
Problem: A heat engine absorbs 1000 J from a hot reservoir at 500 K and rejects 600 J to a cold reservoir at 300 K. Find actual and maximum possible efficiency.
Solution:
Given: Q_H = 1000 J, Q_C = 600 J, T_H = 500 K, T_C = 300 K
Actual efficiency:
η_actual = (Q_H - Q_C)/Q_H = (1000 - 600)/1000 = 0.4 = 40%
Maximum efficiency (Carnot):
η_max = 1 - T_C/T_H = 1 - 300/500 = 0.4 = 40%
This engine is operating at maximum theoretical efficiency!Cyclic Process
Definition
A cyclic process is a thermodynamic process where the system returns to its initial state after completing the process. All state variables return to their original values.
Characteristics
- Net change in internal energy: ΔU = 0
- First law becomes: Q = W (heat supplied equals work done)
- Forms closed loop on P-V diagram
- Repeatable process
Types of Cycles
- Carnot Cycle: Most efficient theoretical cycle
- Otto Cycle: Gasoline engines
- Diesel Cycle: Diesel engines
- Brayton Cycle: Gas turbines
Mathematical Relations
∮ dU = 0 (internal energy returns to initial value)
∮ dQ = ∮ dW (total heat = total work)Work Done in Cycle
Work done = Area enclosed by the cycle on P-V diagram
Example
A gas undergoes a cyclic process: expansion → cooling → compression → heating
- Net ΔU = 0
- Net work = area of loop on P-V diagram
Constant Pressure (Isobaric) Process
Definition
An isobaric process is one where pressure remains constant throughout the process.
Characteristics
- Pressure: P = constant
- Work done: W = P × ΔV = P(V₂ - V₁)
- First law: ΔU = Q - PΔV
Ideal Gas Relations
V₁/T₁ = V₂/T₂ (Charles's Law)
V ∝ T (at constant P)Work Done
W = ∫ P dV = P ∫ dV = P(V₂ - V₁)Heat Capacity
At constant pressure: Q = nCₚΔT
Where Cₚ = molar heat capacity at constant pressure
Example Problem
Problem: 2 moles of ideal gas at 2 atm expand isobarically from 10 L to 20 L. Find work done.
Solution:
Given: n = 2 mol, P = 2 atm = 2 × 10⁵ Pa, V₁ = 10 L, V₂ = 20 L
W = P(V₂ - V₁) = 2 × 10⁵ × (20 - 10) × 10⁻³
W = 2 × 10⁵ × 10 × 10⁻³ = 2000 JP-V Diagram
Horizontal line (constant pressure)
Constant Volume (Isochoric) Process
Definition
An isochoric process is one where volume remains constant throughout the process.
Characteristics
- Volume: V = constant
- Work done: W = 0 (no volume change)
- First law: ΔU = Q (all heat goes to internal energy)
Ideal Gas Relations
P₁/T₁ = P₂/T₂ (Gay-Lussac's Law)
P ∝ T (at constant V)Heat Capacity
At constant volume: Q = nCᵥΔT
Where Cᵥ = molar heat capacity at constant volume
Key Points
- No work done since dV = 0
- All supplied heat increases internal energy
- Pressure changes with temperature
Example Problem
Problem: Gas at 300 K and 1 atm is heated at constant volume to 600 K. Find final pressure.
Solution:
Given: T₁ = 300 K, P₁ = 1 atm, T₂ = 600 K, V = constant
Using P₁/T₁ = P₂/T₂:
P₂ = P₁ × (T₂/T₁) = 1 × (600/300) = 2 atmP-V Diagram
Vertical line (constant volume)
Slopes and Work
Definition
This section covers the slopes of isothermal and adiabatic curves on P-V diagrams and the work done in adiabatic processes. Understanding these slopes helps differentiate between different thermodynamic processes graphically.
Slope of Isotherm
On a P-V diagram, the slope of an isothermal curve is:
dP/dV = -P/V = -nRT/V²Slope of Adiabatic
For an adiabatic process:
dP/dV = -γP/VComparison
- Adiabatic curves are steeper than isothermal curves
- Ratio of slopes:
(dP/dV)_adiabatic/(dP/dV)_isothermal = γ
Work Done in Adiabatic Process
Definition: Work done in an adiabatic process where no heat is exchanged (Q = 0).
Primary Formula:
W = (P₁V₁ - P₂V₂)/(γ - 1)Alternative Forms:
W = nCᵥ(T₁ - T₂) (using temperature)
W = (nRT₁ - nRT₂)/(γ - 1) (using ideal gas law)From First Law: Since Q = 0 in adiabatic process:
ΔU = -W
W = -ΔU = -nCᵥΔT = nCᵥ(T₁ - T₂)Key Points:
- Work comes from internal energy of the gas
- Temperature decreases during adiabatic expansion
- Temperature increases during adiabatic compression
- More work is required for adiabatic compression than isothermal
Example Problem: Problem: 2 moles of ideal gas (γ = 1.4, Cᵥ = 5R/2) expand adiabatically from 300 K to 250 K. Find work done.
Solution:
Given: n = 2 mol, T₁ = 300 K, T₂ = 250 K, γ = 1.4
Cᵥ = 5R/2 = 5 × 8.314/2 = 20.785 J/(mol·K)
W = nCᵥ(T₁ - T₂)
W = 2 × 20.785 × (300 - 250)
W = 2 × 20.785 × 50 = 2078.5 J
Work done by the gas = 2078.5 JFirst Law of Thermodynamics (Enhanced)
Definition
The First Law of Thermodynamics is the law of energy conservation applied to thermodynamic systems. Energy cannot be created or destroyed, only converted from one form to another.
Mathematical Statement
ΔU = Q - WWhere:
- ΔU = change in internal energy of the system
- Q = heat added to the system (+) or removed (-)
- W = work done by the system (+) or on the system (-)
Alternative Forms
Q = ΔU + W (heat supplied = change in internal energy + work done by system)
dU = δQ - δW (differential form)Sign Conventions
- Heat (Q): Positive if added to system, negative if removed
- Work (W): Positive if done by system (expansion), negative if done on system (compression)
- Internal Energy (ΔU): Positive if increased, negative if decreased
Applications to Different Processes
Isothermal Process (ΔT = 0):
- ΔU = 0, so Q = W
- All heat goes into work
Adiabatic Process (Q = 0):
- ΔU = -W
- Work comes from internal energy
Isochoric Process (W = 0):
- ΔU = Q
- All heat changes internal energy
Isobaric Process:
- ΔU = Q - PΔV
- Heat goes to both internal energy and work
Example Problem
Problem: A gas absorbs 500 J of heat and does 200 J of work during expansion. Find the change in internal energy.
Solution:
Given: Q = +500 J (heat added), W = +200 J (work by system)
Using First Law: ΔU = Q - W
ΔU = 500 - 200 = 300 J
Internal energy increases by 300 J.Physical Significance
- Energy is conserved in all thermodynamic processes
- Heat and work are different ways of transferring energy
- Internal energy is a state function (path independent)
- Heat and work are path functions (path dependent)
Carnot Cycle
Definition
The Carnot cycle is a theoretical thermodynamic cycle that provides maximum efficiency for any heat engine operating between two thermal reservoirs.
Four Processes
- Isothermal expansion (A→B): Heat Qₕ absorbed from hot reservoir
- Adiabatic expansion (B→C): Temperature drops from Tₕ to Tc
- Isothermal compression (C→D): Heat Qc rejected to cold reservoir
- Adiabatic compression (D→A): Temperature rises from Tc to Tₕ
Carnot Efficiency
η = 1 - Tc/Tₕ = 1 - Qc/QₕWhere:
- Tₕ = temperature of hot reservoir (K)
- Tc = temperature of cold reservoir (K)
Work Output
W = Qₕ - Qc = Qₕ(1 - Tc/Tₕ)Example Problem
Problem: A Carnot engine operates between reservoirs at 500 K and 300 K. If it absorbs 1000 J from hot reservoir, find efficiency and work output.
Solution:
Given: Tₕ = 500 K, Tc = 300 K, Qₕ = 1000 J
Efficiency:
η = 1 - Tc/Tₕ = 1 - 300/500 = 1 - 0.6 = 0.4 = 40%
Work output:
W = ηQₕ = 0.4 × 1000 = 400 J
Heat rejected:
Qc = Qₕ - W = 1000 - 400 = 600 JRefrigeration Cycle
Definition
A refrigeration cycle is the reverse of a heat engine - it removes heat from a cold reservoir and rejects it to a hot reservoir, requiring work input.
Coefficient of Performance (COP)
For refrigerator:
COP_R = Qc/W = Qc/(Qₕ - Qc)For heat pump:
COP_HP = Qₕ/W = Qₕ/(Qₕ - Qc)Carnot Refrigerator
Maximum theoretical COP:
COP_R = Tc/(Tₕ - Tc)
COP_HP = Tₕ/(Tₕ - Tc)Relationship
COP_HP = COP_R + 1Four Processes (Reverse Carnot)
- Adiabatic compression: Work input, temperature rises
- Isothermal compression: Heat rejected to hot reservoir
- Adiabatic expansion: Temperature drops
- Isothermal expansion: Heat absorbed from cold reservoir
Example Problem
Problem: A Carnot refrigerator operates between 250 K and 300 K. Find COP if it removes 500 J from cold reservoir.
Solution:
Given: Tc = 250 K, Tₕ = 300 K, Qc = 500 J
COP_R = Tc/(Tₕ - Tc) = 250/(300 - 250) = 250/50 = 5
Work required:
W = Qc/COP_R = 500/5 = 100 J
Heat rejected to hot reservoir:
Qₕ = Qc + W = 500 + 100 = 600 JQuick Reference Formulas
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A. Waves and Oscillations (Section)
Basic Wave Properties:
v = fλ(wave speed)T = 1/f(period)ω = 2πf = 2π/T(angular frequency)
Periodic Motion: (Section)
x(t + T) = x(t)(condition for periodicity)
B. Simple Harmonic Motion (SHM) (Section)
Fundamental Relations:
F = -kx(Hooke's Law)a = -ω²x(acceleration)ω = 2πf = 2π/T = √(k/m)(angular frequency for spring-mass)
Motion Equations:
x(t) = A cos(ωt + φ)(displacement)v(t) = -Aω sin(ωt + φ)(velocity leads displacement by π/2)a(t) = -Aω² cos(ωt + φ) = -ω²x(acceleration opposes displacement)
Key Relationships: (Section)
v² = ω²(A² - x²)(velocity-displacement relation)v_max = Aω(maximum velocity at equilibrium)a_max = Aω²(maximum acceleration at extremes)A = √(x₀² + (v₀/ω)²)(amplitude from initial conditions)
C. Energy in Oscillations
Energy Conservation: (Section)
E_total = (1/2)kA² = constantE = KE + PE = (1/2)mv² + (1/2)kx²
Kinetic Energy: (Section)
KE = (1/2)mv²KE = (1/2)k(A² - x²)KE_max = (1/2)kA²(at equilibrium)
Potential Energy: (Section)
PE = (1/2)kx²PE_max = (1/2)kA²(at extremes)
D. Pendulums
Simple Pendulum: (Section)
T = 2π√(L/g)(period, independent of mass for small angles)ω = √(g/L)(angular frequency)f = (1/2π)√(g/L)(frequency)
Pendulum in Lift: (Section)
g_eff = g + a(upward acceleration)g_eff = g - a(downward acceleration)T = 2π√(L/g_eff)(modified period)
Physical Pendulum: (Section)
T = 2π√(I/mgd)(period)I = I_cm + md²(parallel axis theorem)
E. Rotational Mechanics
Center of Mass: (Section)
x_cm = (Σmᵢxᵢ)/(Σmᵢ)(discrete masses)x_cm = (1/M) ∫ x dm(continuous distribution)
Torque and Moment of Inertia: (Section)
τ = r × F = rF sin θ(torque)τ = Iα(rotational Newton's 2nd law)I = Σ mᵢrᵢ²(discrete masses)I = ∫ r² dm(continuous distribution)
Common Moments of Inertia:
- Solid sphere (center):
I = (2/5)MR² - Solid cylinder (axis):
I = (1/2)MR² - Rod (center):
I = (1/12)ML² - Rod (end):
I = (1/3)ML²
Linear vs Circular Motion: (Section)
- Linear:
F = ma, Rotational:τ = Iα v ↔ ω,a ↔ α,m ↔ I,F ↔ τ,x ↔ θ
F. Thermodynamics Fundamentals
Ideal Gas Laws: (Section)
PV = nRT(ideal gas equation, R = 8.314 J/(mol·K))PV = constant(Boyle's Law, constant T)V/T = constant(Charles's Law, constant P)P/T = constant(Gay-Lussac's Law, constant V)(P₁V₁)/T₁ = (P₂V₂)/T₂(combined gas law)
First Law of Thermodynamics: (Section)
ΔU = Q - W(energy conservation)Q = ΔU + W(alternative form)- Sign convention: Q > 0 (heat in), W > 0 (work by system)
Efficiency: (Section)
η = W_out/Q_in = (Q_H - Q_C)/Q_H(heat engine)η_max = 1 - T_C/T_H(Carnot efficiency)
G. Thermodynamic Processes
Isothermal Process: (Section)
T = constant,ΔU = 0,Q = WPV = constant,P₁V₁ = P₂V₂W = nRT ln(V₂/V₁) = nRT ln(P₁/P₂)
Adiabatic Process: (Section)
Q = 0,ΔU = -WPVᵞ = constant,TVᵞ⁻¹ = constant,TPᵞ⁻¹/ᵞ = constantW = (P₁V₁ - P₂V₂)/(γ-1) = nCᵥ(T₁ - T₂)
Isobaric Process: (Section)
P = constant,V/T = constantW = PΔV = P(V₂ - V₁)Q = nCₚΔT,ΔU = Q - PΔV
Isochoric Process: (Section)
V = constant,P/T = constant,W = 0ΔU = Q = nCᵥΔT
Slopes and Work: (Section)
- Isothermal slope:
dP/dV = -P/V - Adiabatic slope:
dP/dV = -γP/V - Adiabatic curves are steeper by factor γ
Reversible Process: (Section)
- Quasi-static, no friction, maximum efficiency
dS_universe = 0
H. Thermodynamic Cycles
Cyclic Process: (Section)
ΔU = 0(returns to initial state)Q_net = W_net(total heat = total work)- Work = area enclosed on P-V diagram
Carnot Cycle: (Section)
- Four processes: isothermal expansion → adiabatic expansion → isothermal compression → adiabatic compression
η = 1 - T_C/T_H = 1 - Q_C/Q_H- Maximum theoretical efficiency
Refrigeration Cycle: (Section)
COP_R = Q_C/W = T_C/(T_H - T_C)(refrigerator)COP_HP = Q_H/W = T_H/(T_H - T_C)(heat pump)COP_HP = COP_R + 1
Important Constants
g = 9.8 m/s²(acceleration due to gravity)R = 8.314 J/(mol·K)(universal gas constant)γ = Cₚ/Cᵥ(adiabatic index: ~1.4 for diatomic gases, ~1.67 for monatomic)Cᵥ = R/(γ-1)(molar heat capacity at constant volume)Cₚ = γR/(γ-1)(molar heat capacity at constant pressure)
Final Exam Practice Questions
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Question 1: Simple Harmonic Motion and Energy
A mass of 2.0 kg is attached to a horizontal spring with spring constant k = 800 N/m. The mass is displaced 0.15 m from its equilibrium position and released from rest. The surface is frictionless.
(a) Calculate the angular frequency, frequency, and period of oscillation.
(b) Find the maximum velocity and maximum acceleration of the mass.
(c) When the displacement is 0.10 m from equilibrium, calculate:
- (i) The velocity of the mass
- (ii) The kinetic energy
- (iii) The potential energy
(d) Write the equations for displacement x(t), velocity v(t), and acceleration a(t) as functions of time, assuming the mass starts from maximum displacement.
Solution 1:
(a) Angular frequency, frequency, and period:
Given: m = 2.0 kg, k = 800 N/m, A = 0.15 m
Angular frequency: ω = √(k/m) = √(800/2.0) = √400 = 20 rad/s
Frequency: f = ω/(2π) = 20/(2π) = 3.18 Hz
Period: T = 1/f = 2π/ω = 2π/20 = 0.314 s(b) Maximum velocity and acceleration:
Maximum velocity (at equilibrium):
v_max = Aω = 0.15 × 20 = 3.0 m/s
Maximum acceleration (at extremes):
a_max = Aω² = 0.15 × 20² = 0.15 × 400 = 60 m/s²(c) At x = 0.10 m:
(i) Velocity:
Using v² = ω²(A² - x²)
v² = 20²(0.15² - 0.10²) = 400(0.0225 - 0.01) = 400(0.0125) = 5
v = ±2.24 m/s
(ii) Kinetic energy:
KE = ½mv² = ½ × 2.0 × 5 = 5.0 J
(iii) Potential energy:
PE = ½kx² = ½ × 800 × 0.10² = 400 × 0.01 = 4.0 J
Check: Total energy = KE + PE = 5.0 + 4.0 = 9.0 J
E_total = ½kA² = ½ × 800 × 0.15² = 9.0 J ✓(d) Equations of motion:
Starting from maximum displacement (x₀ = A, v₀ = 0):
x(t) = 0.15 cos(20t) m
v(t) = -3.0 sin(20t) m/s
a(t) = -60 cos(20t) m/s²Question 2: Thermodynamic Cycle Analysis
An ideal gas undergoes a cyclic process consisting of four stages:
- Process A→B: Isothermal expansion at 400 K from 2.0 L to 8.0 L
- Process B→C: Adiabatic expansion (γ = 1.4) until temperature drops to 300 K
- Process C→D: Isothermal compression at 300 K
- Process D→A: Adiabatic compression back to initial state
The gas contains 0.5 moles.
(a) For process A→B, calculate:
- (i) Initial and final pressures
- (ii) Work done by the gas
- (iii) Heat absorbed
(b) For process B→C, find the final volume and work done.
(c) Calculate the efficiency of this heat engine.
(d) Compare this efficiency with the maximum possible Carnot efficiency between the same temperature limits.
Solution 2:
(a) Process A→B (Isothermal at 400 K):
Given: n = 0.5 mol, T = 400 K, V₁ = 2.0 L, V₂ = 8.0 L
R = 8.314 J/(mol·K)
(i) Pressures:
Initial: P₁ = nRT/V₁ = (0.5)(8.314)(400)/(2.0×10⁻³) = 831,400 Pa ≈ 8.31 atm
Final: P₂ = nRT/V₂ = (0.5)(8.314)(400)/(8.0×10⁻³) = 207,850 Pa ≈ 2.08 atm
(ii) Work done:
W = nRT ln(V₂/V₁) = (0.5)(8.314)(400) ln(8.0/2.0)
W = 1662.8 × ln(4) = 1662.8 × 1.386 = 2305 J
(iii) Heat absorbed:
For isothermal process: ΔU = 0, so Q = W = 2305 J(b) Process B→C (Adiabatic expansion):
From 400 K to 300 K, starting at V = 8.0 L
Using TV^(γ-1) = constant:
T₁V₁^(γ-1) = T₂V₂^(γ-1)
400 × (8.0)^0.4 = 300 × V₂^0.4
V₂^0.4 = 400 × (8.0)^0.4 / 300 = 1.333 × 2.297 = 3.063
V₂ = (3.063)^2.5 = 12.67 L
Work done: W = nCᵥ(T₁ - T₂)
For ideal gas: Cᵥ = R/(γ-1) = 8.314/0.4 = 20.785 J/(mol·K)
W = (0.5)(20.785)(400 - 300) = 1039 J(c) Efficiency calculation:
Heat absorbed (from hot reservoir) = Q_AB = 2305 J
For complete cycle, need to find heat rejected at low temperature.
Process C→D: Isothermal compression at 300 K
Process D→A: Adiabatic compression
By symmetry and energy conservation:
Q_CD = -nRT_cold ln(V_D/V_C)
For Carnot-like cycle efficiency:
η = 1 - T_cold/T_hot = 1 - 300/400 = 0.25 = 25%(d) Carnot efficiency comparison:
Maximum Carnot efficiency:
η_Carnot = 1 - T_C/T_H = 1 - 300/400 = 0.25 = 25%
This cycle achieves the maximum theoretical efficiency because it operates
between the same temperature limits with reversible processes.Question 3: Coupled Pendulum System
A physical pendulum consists of a uniform rod of length L = 1.2 m and mass M = 3.0 kg, pivoted at a point 0.3 m from one end. The pendulum is inside an elevator.
(a) Calculate the period of small oscillations when the elevator is:
- (i) At rest
- (ii) Accelerating upward at 2.0 m/s²
(b) A point mass m = 0.5 kg is attached at the free end of the rod. How does this change the period when the elevator is at rest?
(c) If the pendulum is displaced by 5° and released, find the maximum angular velocity and maximum angular acceleration for case (a)(i).
Solution 3:
(a) Period calculations:
Given: L = 1.2 m, M = 3.0 kg, pivot at 0.3 m from end
Distance from pivot to center of mass: d = 0.6 - 0.3 = 0.3 m
Moment of inertia about center: I_cm = ML²/12 = 3.0 × (1.2)²/12 = 0.36 kg·m²
Moment of inertia about pivot: I = I_cm + Md² = 0.36 + 3.0 × (0.3)² = 0.63 kg·m²
(i) At rest (g = 9.8 m/s²):
T = 2π√(I/Mgd) = 2π√(0.63/(3.0 × 9.8 × 0.3))
T = 2π√(0.63/8.82) = 2π√(0.0714) = 2π × 0.267 = 1.68 s
(ii) Accelerating upward (g_eff = 9.8 + 2.0 = 11.8 m/s²):
T = 2π√(0.63/(3.0 × 11.8 × 0.3)) = 2π√(0.63/10.62)
T = 2π√(0.0593) = 2π × 0.244 = 1.53 s(b) With additional mass:
New center of mass location:
x_cm = (M × 0.6 + m × 1.2)/(M + m) = (3.0 × 0.6 + 0.5 × 1.2)/(3.5) = 0.686 m from original end
New d = 0.686 - 0.3 = 0.386 m
New moment of inertia:
I_new = I_rod + m × (1.2 - 0.3)² = 0.63 + 0.5 × (0.9)² = 1.035 kg·m²
New period:
T = 2π√(1.035/(3.5 × 9.8 × 0.386)) = 2π√(0.781) = 1.76 s(c) Maximum angular velocity and acceleration:
θ₀ = 5° = 5π/180 = 0.0873 rad
For small oscillations: θ(t) = θ₀ cos(ωt)
ω = √(Mgd/I) = √(8.82/0.63) = 3.74 rad/s
Maximum angular velocity:
ω_max = θ₀ × ω = 0.0873 × 3.74 = 0.326 rad/s
Maximum angular acceleration:
α_max = θ₀ × ω² = 0.0873 × (3.74)² = 1.22 rad/s²Question 4: Combined Heat Engine and Oscillation
A Carnot heat engine operates between reservoirs at 500 K and 300 K. The engine drives a compressor that compresses a spring with spring constant k = 2000 N/m. The compressed spring then drives a 1.0 kg mass in simple harmonic motion.
(a) If the heat engine absorbs 1000 J from the hot reservoir per cycle, calculate:
- (i) The efficiency
- (ii) Work output per cycle
- (iii) Heat rejected to cold reservoir
(b) The work output compresses the spring by 0.20 m from its natural length. When released, this drives the 1.0 kg mass. Find:
- (i) The amplitude of oscillation
- (ii) The frequency of oscillation
- (iii) The maximum speed of the mass
(c) If 10% of the kinetic energy is lost to friction during each oscillation, how many complete oscillations will occur before the amplitude drops to half its initial value?
Solution 4:
(a) Carnot engine analysis:
Given: T_H = 500 K, T_C = 300 K, Q_H = 1000 J
(i) Efficiency:
η = 1 - T_C/T_H = 1 - 300/500 = 0.4 = 40%
(ii) Work output:
W = η × Q_H = 0.4 × 1000 = 400 J
(iii) Heat rejected:
Q_C = Q_H - W = 1000 - 400 = 600 J(b) Spring-mass system:
Given: k = 2000 N/m, m = 1.0 kg, compression = 0.20 m
Work stored in spring = 400 J (from engine)
(i) Amplitude:
Initial potential energy = ½kx² = ½ × 2000 × (0.20)² = 40 J
But total energy available = 400 J
So: ½kA² = 400 J
A² = 800/2000 = 0.4
A = 0.632 m
(ii) Frequency:
ω = √(k/m) = √(2000/1.0) = 44.7 rad/s
f = ω/(2π) = 44.7/(2π) = 7.11 Hz
(iii) Maximum speed:
v_max = Aω = 0.632 × 44.7 = 28.3 m/s(c) Energy loss analysis:
Initial energy: E₀ = 400 J
After each cycle: E_new = 0.9 × E_old (10% loss)
Energy is proportional to A²:
E ∝ A²
For amplitude to drop to A/2:
Final energy = E₀/4 = 100 J
Using: E_n = E₀ × (0.9)ⁿ
100 = 400 × (0.9)ⁿ
0.25 = (0.9)ⁿ
ln(0.25) = n × ln(0.9)
n = ln(0.25)/ln(0.9) = -1.386/(-0.105) = 13.2
Therefore, approximately 13 complete oscillations.Question 5: Coupled Oscillations and Thermodynamics
A system consists of a simple pendulum (length L = 1.5 m, mass m = 2.0 kg) attached to a piston that compresses an ideal gas in a cylinder. The gas contains 0.5 moles with γ = 1.4, initially at 300 K and 2.0 atm pressure, occupying 3.0 L volume.
(a) For the pendulum oscillations:
- (i) Calculate the period of small oscillations in Earth's gravity
- (ii) Find the maximum speed if the pendulum is displaced 10° from vertical
- (iii) Calculate the total mechanical energy of the pendulum
(b) The gas undergoes a thermodynamic cycle as the pendulum oscillates:
- (i) If the gas expands isothermally to 6.0 L, find the final pressure and work done
- (ii) The gas then undergoes adiabatic expansion until the temperature drops to 250 K. Find the final volume
- (iii) Calculate the efficiency if this system operates as a heat engine between these temperature limits
(c) The entire system is placed in an elevator accelerating upward at 4.0 m/s²:
- (i) Find the new period of the pendulum
- (ii) How does this acceleration affect the gas pressure if volume remains constant?
- (iii) Calculate the new equilibrium position of the pendulum
(d) Advanced analysis:
- (i) If the pendulum bob is replaced with a uniform rod of the same mass and length L, find the new period
- (ii) Calculate the center of mass of the rod-pendulum system
- (iii) Determine the moment of inertia about the pivot point
Solution 5:
(a) Pendulum oscillations:
Given: L = 1.5 m, m = 2.0 kg, θ₀ = 10° = 0.175 rad
(i) Period of small oscillations:
T = 2π√(L/g) = 2π√(1.5/9.8) = 2π√(0.153) = 2π × 0.391 = 2.46 s
(ii) Maximum speed:
For small oscillations: ω = √(g/L) = √(9.8/1.5) = 2.56 rad/s
v_max = θ₀ × ω × L = 0.175 × 2.56 × 1.5 = 0.672 m/s
(iii) Total mechanical energy:
E = ½mgh = ½mg(L - L cos θ₀) = ½mgL(1 - cos θ₀)
E = ½ × 2.0 × 9.8 × 1.5 × (1 - cos 10°) = 14.7 × (1 - 0.985) = 0.221 J(b) Thermodynamic cycle:
Given: n = 0.5 mol, γ = 1.4, T₁ = 300 K, P₁ = 2.0 atm, V₁ = 3.0 L
(i) Isothermal expansion to V₂ = 6.0 L:
P₂ = P₁V₁/V₂ = 2.0 × 3.0/6.0 = 1.0 atm
W = nRT ln(V₂/V₁) = 0.5 × 8.314 × 300 × ln(2) = 865 J
(ii) Adiabatic expansion to T₃ = 250 K:
Using TV^(γ-1) = constant:
V₃ = V₂(T₂/T₃)^(1/(γ-1)) = 6.0 × (300/250)^(1/0.4) = 6.0 × (1.2)^2.5 = 8.79 L
(iii) Heat engine efficiency:
η_max = 1 - T_cold/T_hot = 1 - 250/300 = 0.167 = 16.7%(c) In accelerating elevator (a = 4.0 m/s²):
Effective gravity: g_eff = g + a = 9.8 + 4.0 = 13.8 m/s²
(i) New period:
T_new = 2π√(L/g_eff) = 2π√(1.5/13.8) = 2π√(0.109) = 2.07 s
(ii) Gas pressure at constant volume:
The acceleration doesn't directly affect gas pressure if volume is fixed
and temperature remains constant. P remains ≈ 2.0 atm
(iii) New equilibrium position:
The pendulum equilibrium doesn't change - it still hangs vertically
relative to the effective gravity direction.(d) Physical pendulum analysis:
(i) Rod pendulum (uniform rod, mass m = 2.0 kg, length L = 1.5 m):
Moment of inertia about end: I = ⅓mL² = ⅓ × 2.0 × (1.5)² = 1.5 kg·m²
Distance to center of mass: d = L/2 = 0.75 m
T = 2π√(I/mgd) = 2π√(1.5/(2.0×9.8×0.75)) = 2π√(0.102) = 2.01 s
(ii) Center of mass:
For uniform rod: Located at geometric center, L/2 = 0.75 m from pivot
(iii) Moment of inertia about pivot:
I = ⅓mL² = ⅓ × 2.0 × (1.5)² = 1.5 kg·m²Tips for the Exam
- Remember the signs: In Simple Harmonic Motion (SHM), acceleration is always opposite to displacement
- Energy conservation: Total mechanical energy is constant in Simple Harmonic Motion (SHM)
- Small angle approximation: For pendulums, sin θ ≈ θ when θ < 15°
- Units: Always check units in your final answers
- Graphs: Practice sketching x-t, v-t, and a-t graphs for Simple Harmonic Motion (SHM)
- Thermodynamic processes: Remember Q = 0 for adiabatic, T = constant for isothermal
- Carnot efficiency: It's the maximum possible efficiency between two reservoirs
- Multi-part questions: Read all parts before starting - later parts often give clues for earlier ones
- Show all work: Partial credit is often awarded for correct methodology
- Check reasonableness: Do your answers make physical sense?