Physics CSS Solved Papers

CSS Physics Paper-I 2025 Solved

Engr. Muhammad Yar Saqib

CSS Physics Paper-I 2025 Solved is a complete solved guide for CSS aspirants who need real answers, not only topic hints. This post solves the subjective section question by question with definitions, derivations, formulas, numerical substitutions, final results and exam-ready explanations. It covers Stokes theorem, conservative vector fields, line integral of gradient, velocity and acceleration components, Fermi-Dirac statistics, Bose-Einstein statistics, Maxwell-Boltzmann statistics, classical and quantum statistical mechanics, paddle-wheel work, pressure rise in a vessel, viscosity, capillarity, nozzle continuity, double slit interference, grating resolving power, SHM acceleration and velocity, Carnot cycle, Gibbs free energy, heat engine efficiency, Clausius-Clapeyron equation, adiabatic relation, isothermal work, Newton’s rings, polarization by reflection and Doppler effect.

Central Argument: A CSS Physics solved paper should not only identify the topic asked in the paper. It should define the concept, derive the formula, substitute the values and explain the physical meaning. Therefore, this CSS Physics Paper-I 2025 Solved post gives the complete route to each answer so students can reproduce the solution in the examination hall.

Scan Note: The uploaded text contains a few distorted symbols. In Q2(c), the curve is interpreted as x=2t², y=t²-4t, z=3t-5. In Q7(b), the printed relation is interpreted as the standard adiabatic result TV^(γ-1)=constant. In Q7(c), the pressure is interpreted as 2.04×10⁵ Pa. These assumptions are stated clearly inside the solutions.

CSS Physics Paper-I 2025 Solved Study Scope

This post covers CSS Physics Paper-I 2025 Solved in a complete, structured and WordPress-ready format. Each question includes the printed question, part-wise solution, important formulas, mathematical working, final answer and examiner-friendly explanation.

Use this solved paper as a study document. First revise the formula sheet, then read Q2 to Q8 one by one. After reading, close the post and rewrite each solution from memory. CSS Physics rewards clear assumptions, correct formulas, clean derivations, correct units and disciplined presentation.

Show Table of Contents
  1. Overview
  2. Study Scope
  3. Important Formula Sheet
  4. Question Map
  5. Question 2: Stokes Theorem, Conservative Field, Velocity and Acceleration
  6. Question 3: Quantum Statistics and Pressure After Paddle-Wheel Work
  7. Question 4: Viscosity, Capillarity and Nozzle Continuity
  8. Question 5: Double Slit, Grating Resolving Power and SHM
  9. Question 6: Carnot Cycle, Gibbs Function and Heat Engine Efficiency
  10. Question 7: Clausius-Clapeyron, Adiabatic Relation and Isothermal Work
  11. Question 8: Newton’s Rings, Polarization by Reflection and Doppler Effect
  12. Revision Plan
  13. Internal and External Resources
  14. FAQs

Important Formula Sheet for CSS Physics Paper-I 2025 Solved

Vector Calculus

∮C A·dl = ∬S (∇×A)·n dS

A = ∇φ ⇒ ∮ A·dl = 0

v = dr/dt

a = d²r/dt²

Fluids and SHM

τ = η dv/dy

Q = Av

h = 2Tcosθ/(ρgr)

a = -ω²x

v = ω√(A²-x²)

Optics and Waves

I = I1 + I2 + 2√(I1I2)cosδ

I = 4I0 cos²(δ/2)

R = λ/Δλ = mN

tanθB = n2/n1

Thermodynamics

η = W/QH

W = QH - QC

dP/dT = L/[T(V2-V1)]

TV^(γ-1)=constant

W = nRT ln(V2/V1)

Question Map of CSS Physics Paper-I 2025 Solved

Question Main Area What Is Fully Solved
Q2 Vector calculus and kinematics Stokes theorem, closed line integral of gradient field, velocity and acceleration components along a given direction.
Q3 Statistical mechanics and thermodynamics Three statistics, classical vs quantum statistical mechanics, pressure rise after paddle-wheel work.
Q4 Fluid mechanics Viscosity, temperature effect on liquids and gases, capillary rise/depression, nozzle diameter and flow rate.
Q5 Optics and oscillations Double slit interference intensity, maxima/minima, grating resolving power, SHM velocity and acceleration.
Q6 Thermodynamics Carnot cycle, Gibbs function, reversible isothermal-isobaric process, heat engine work and efficiency.
Q7 Thermodynamics and phase change Clausius-Clapeyron equation, adiabatic relation, isothermal expansion and constant-pressure cooling work.
Q8 Wave optics and sound Newton’s rings, polarization by reflection, Doppler effect notes.

Question 2: Stokes Theorem, Conservative Field, Velocity and Acceleration

Full Question

Q.2. (a) State and prove Stoke’s theorem.

Q.2. (b) Prove that if the vector is the gradient of a scalar function, then its line integral around a closed curve is zero.

Q.2. (c) A particle moves along the curve x=2t², y=t²-4t, z=3t-5, where t is the time. Find the components of its velocity and acceleration at time t=1 in the direction 2i-3j+2k.

Q2(a): Statement of Stokes Theorem

Stokes theorem states that the line integral of a vector field around a closed curve is equal to the surface integral of the curl of that vector field over any open surface bounded by the curve.

∮C A · dl = ∬S (∇ × A) · n dS

Here, C is the closed boundary curve, S is the surface bounded by C, A is the vector field, dl is a line element along the closed curve, and n is the unit normal to the surface.

Proof of Stokes Theorem

Consider a smooth surface S bounded by a closed curve C. Divide the surface into a large number of small surface elements. For one small element, the circulation of the vector field around its boundary is approximately equal to the normal component of the curl times the small area:

small circulation = (∇ × A) · n ΔS

Now add the circulation over all small elements. The line integrals along internal boundaries cancel because each internal boundary is traversed twice in opposite directions by neighbouring elements. Therefore, only the outer boundary curve C remains.

Σ small circulations = ∮C A · dl

The sum of all curl fluxes becomes the surface integral over S:

Σ (∇ × A) · n ΔS = ∬S (∇ × A) · n dS

Hence:

∮C A · dl = ∬S (∇ × A) · n dS
Result: This proves Stokes theorem.

Physical Significance of Stokes Theorem

Stokes theorem connects circulation around a closed boundary with rotation of a field over the surface bounded by that boundary. It is widely used in electromagnetism, fluid mechanics and vector calculus. Maxwell’s equations in integral and differential form are connected through Stokes theorem.

Q2(b): Line Integral of a Gradient Field Around a Closed Curve

Let a vector field A be the gradient of a scalar function φ:

A = ∇φ

The line integral of A around a closed curve is:

∮ A · dl = ∮ ∇φ · dl

But:

∇φ · dl = dφ

Therefore:

∮ A · dl = ∮ dφ

When we move around a closed curve, the initial and final points are the same. Therefore, the scalar function returns to its original value:

∮ dφ = φfinal – φinitial = 0

Hence:

∮ A · dl = 0
Final Answer for Q2(b): If A=∇φ, then ∮A·dl=0. A gradient field is conservative, and its closed line integral is zero.

Q2(c): Velocity and Acceleration Components Along Given Direction

Assumption: The uploaded scan writes the curve in distorted form. The solution uses the interpreted equations: x=2t², y=t²-4t, z=3t-5.

The position vector is:

r(t) = x i + y j + z k
r(t) = 2t² i + (t² – 4t)j + (3t – 5)k

Velocity

Velocity is the first derivative of position:

v = dr/dt
v = 4t i + (2t – 4)j + 3k

At t=1:

v(1) = 4i + (2-4)j + 3k
v(1) = 4i – 2j + 3k

Acceleration

Acceleration is the derivative of velocity:

a = dv/dt
a = 4i + 2j + 0k

At t=1, acceleration is still:

a(1) = 4i + 2j

Component Along the Direction 2i – 3j + 2k

The direction vector is:

u = 2i – 3j + 2k

Magnitude of u is:

|u| = √(2² + (-3)² + 2²)
|u| = √(4 + 9 + 4)
|u| = √17

Unit vector along the given direction is:

û = (2i – 3j + 2k)/√17

Velocity Component Along u

v · û = (4i – 2j + 3k) · (2i – 3j + 2k)/√17
v · û = [4(2) + (-2)(-3) + 3(2)]/√17
v · û = (8 + 6 + 6)/√17
v · û = 20/√17
v · û ≈ 4.85 m/s

Acceleration Component Along u

a · û = (4i + 2j + 0k) · (2i – 3j + 2k)/√17
a · û = [4(2) + 2(-3) + 0(2)]/√17
a · û = (8 – 6)/√17
a · û = 2/√17
a · û ≈ 0.485 m/s²
Final Answer for Q2(c): At t=1, v=4i-2j+3k and a=4i+2j. Components along 2i-3j+2k are 20/√17 ≈ 4.85 m/s for velocity and 2/√17 ≈ 0.485 m/s² for acceleration.

Question 3: Quantum Statistics and Pressure After Paddle-Wheel Work

Full Question

Q.3. (a) Differentiate between Fermi-Dirac, Bose-Einstein and Maxwell-Boltzmann statistics.

Q.3. (b) What do you understand by classical statistical mechanics and quantum statistical mechanics?

Q.3. (c) A 0.5 m³ vessel is filled with air at atmospheric pressure. The air is churned by a paddle wheel attached to a shaft 0.1 m in diameter, rotating at a speed of 1800 rpm. A force of 5.0 N acts on the rim of the shaft. What would be the pressure in the vessel after 10 s of operation?

Q3(a): Difference Between Fermi-Dirac, Bose-Einstein and Maxwell-Boltzmann Statistics

Statistical mechanics explains how particles are distributed among available energy states. The type of statistics depends on whether the particles are classical or quantum, distinguishable or indistinguishable, and whether Pauli exclusion principle applies.

Feature Maxwell-Boltzmann Statistics Bose-Einstein Statistics Fermi-Dirac Statistics
Type of particles Classical distinguishable particles. Indistinguishable bosons. Indistinguishable fermions.
Spin Classical case; spin is not central. Integer spin: 0, 1, 2, etc. Half-integer spin: 1/2, 3/2, etc.
Pauli exclusion principle Not applicable. Not obeyed. Obeyed.
Particles per state No quantum restriction in classical approximation. Many particles can occupy one quantum state. Only one fermion can occupy one quantum state.
Distribution function f(E)=Ae^(-E/kT) f(E)=1/[e^((E-μ)/kT)-1] f(E)=1/[e^((E-μ)/kT)+1]
Examples Dilute gas molecules at high temperature and low pressure. Photons, phonons, helium-4 atoms. Electrons, protons, neutrons.
Applications Kinetic theory of gases and classical ideal gas. Blackbody radiation, lasers and Bose-Einstein condensation. Electrons in metals, semiconductors and white dwarfs.
Final Answer for Q3(a): Maxwell-Boltzmann statistics is classical and applies to distinguishable particles. Bose-Einstein statistics applies to bosons. Fermi-Dirac statistics applies to fermions and obeys Pauli exclusion principle.

Q3(b): Classical Statistical Mechanics and Quantum Statistical Mechanics

Classical Statistical Mechanics

Classical statistical mechanics studies systems of many particles using classical mechanics. Particles are treated as distinguishable, and their positions and momenta can vary continuously in phase space.

It is suitable for ordinary gases at high temperature and low density, where quantum effects are negligible. Maxwell-Boltzmann distribution is the main example.

Quantum Statistical Mechanics

Quantum statistical mechanics studies many-particle systems using quantum mechanics. Particles are treated as indistinguishable, and energy states are discrete. Quantum statistics also includes spin and the Pauli exclusion principle.

It is necessary for electrons in metals, blackbody radiation, low-temperature gases, semiconductors and nuclear systems.

Classical Statistical Mechanics Quantum Statistical Mechanics
Particles are treated as distinguishable. Identical particles are indistinguishable.
Phase space is continuous. Energy states are quantized.
Uses Maxwell-Boltzmann statistics. Uses Bose-Einstein and Fermi-Dirac statistics.
Valid at high temperature and low density. Important at low temperature, high density or microscopic scale.
Quantum spin is not central. Spin determines whether particles are bosons or fermions.
Final Answer for Q3(b): Classical statistical mechanics deals with distinguishable particles and continuous phase space, while quantum statistical mechanics deals with indistinguishable particles, discrete states and quantum restrictions.

Q3(c): Pressure in Vessel After Paddle-Wheel Work

Given:

Volume of vessel, V = 0.5 m³
Initial pressure, P1 = atmospheric pressure ≈ 101325 Pa
Shaft diameter = 0.1 m
Shaft radius, r = 0.05 m
Force on rim, F = 5.0 N
Speed = 1800 rpm
Time, t = 10 s

Step 1: Torque on Shaft

τ = Fr
τ = 5.0 × 0.05
τ = 0.25 N m

Step 2: Angular Speed

Convert 1800 rpm into revolutions per second:

1800 rpm = 1800/60 = 30 rev/s

Angular speed is:

ω = 2πf
ω = 2π × 30
ω = 188.5 rad/s

Step 3: Work Done by Paddle Wheel

Power delivered is:

P = τω
P = 0.25 × 188.5
P = 47.1 W

Work done in 10 s is:

W = Pt
W = 47.1 × 10
W = 471 J

Step 4: Pressure Rise at Constant Volume

The vessel is closed and volume is constant. Paddle-wheel work increases the internal energy of air. For an ideal gas at constant volume:

ΔU = W

For an ideal gas:

ΔP V = (γ – 1) ΔU

For air:

γ ≈ 1.4

So:

ΔP = (γ – 1)W/V
ΔP = (0.4)(471)/0.5
ΔP = 376.8 Pa

Step 5: Final Pressure

P2 = P1 + ΔP
P2 = 101325 + 376.8
P2 = 101701.8 Pa
P2 ≈ 101.7 kPa
Final Answer for Q3(c): The final pressure in the vessel is approximately 1.017 × 10⁵ Pa, or 101.7 kPa.

Question 4: Viscosity, Capillarity and Nozzle Continuity

Full Question

Q.4. (a) What is viscosity? Discuss effect of temperature on the viscosity of liquids and gases.

Q.4. (b) Explain why the level of mercury is down in a capillary when placed in a container of mercury, while it is up in the capillary in case of water.

Q.4. (c) A garden hose has an inside diameter of 2 cm and water flows through it at 3 m/s. (i) What nozzle diameter is required for the water to emerge at 10 m/s? (ii) At what rate does the water leave the nozzle?

Q4(a): Viscosity

Viscosity is the internal resistance of a fluid to flow. It is caused by friction between adjacent layers of fluid moving with different velocities. A highly viscous fluid flows slowly, while a less viscous fluid flows easily.

Newton’s law of viscosity is:

shear stress = η × velocity gradient
τ = η (dv/dy)

Here, η is the coefficient of viscosity, dv/dy is velocity gradient and τ is shear stress.

Effect of Temperature on Viscosity of Liquids

In liquids, viscosity generally decreases when temperature increases. This happens because cohesive forces between molecules become weaker at higher temperature, allowing layers of liquid to slide more easily.

Examples:

  • Honey flows more easily when heated.
  • Engine oil becomes thinner at high temperature.
  • Water viscosity decreases as temperature rises.

Effect of Temperature on Viscosity of Gases

In gases, viscosity generally increases when temperature increases. This happens because gas molecules move faster at higher temperature and transfer momentum more effectively between layers.

Fluid Type Effect of Temperature Increase Reason
Liquids Viscosity decreases. Cohesive forces weaken.
Gases Viscosity increases. Molecular momentum transfer increases.
Final Answer for Q4(a): Viscosity is internal friction in a fluid. Liquid viscosity decreases with temperature, while gas viscosity increases with temperature.

Q4(b): Mercury Depression and Water Rise in Capillary Tube

Capillarity is the rise or fall of a liquid in a narrow tube due to surface tension and adhesive/cohesive forces.

Water in Glass Capillary

Water rises in a glass capillary because adhesive force between water and glass is greater than cohesive force between water molecules. Therefore, water wets glass and forms a concave meniscus.

For water in glass:

θ < 90°

Therefore:

cosθ positive

So capillary height is positive:

h = 2Tcosθ/(ρgr)

Mercury in Glass Capillary

Mercury is depressed in a glass capillary because cohesive force between mercury atoms is greater than adhesive force between mercury and glass. Therefore, mercury does not wet glass and forms a convex meniscus.

For mercury in glass:

θ > 90°

Therefore:

cosθ negative

So h becomes negative, meaning the level is depressed.

Liquid Meniscus Angle of Contact Capillary Effect
Water Concave θ < 90° Rises in capillary.
Mercury Convex θ > 90° Depressed in capillary.
Final Answer for Q4(b): Water rises because adhesion with glass is stronger than cohesion, while mercury falls because cohesion within mercury is stronger than adhesion with glass.

Q4(c): Nozzle Diameter and Flow Rate

Given:

Hose diameter, d1 = 2 cm = 0.02 m
Hose radius, r1 = 0.01 m
Initial velocity, v1 = 3 m/s
Nozzle velocity, v2 = 10 m/s

Part (i): Nozzle Diameter

For incompressible steady flow, continuity equation is:

A1v1 = A2v2

Since area is proportional to diameter squared:

d1²v1 = d2²v2

Therefore:

d2 = d1 √(v1/v2)

Substitute values:

d2 = 2 cm × √(3/10)
d2 = 2 × √0.3 cm
d2 = 2 × 0.5477 cm
d2 = 1.095 cm
Nozzle diameter: d2 ≈ 1.10 cm.

Part (ii): Rate of Water Leaving the Nozzle

Flow rate is:

Q = A1v1

Area of hose is:

A1 = πr1²
A1 = π(0.01)²
A1 = 3.1416 × 10⁻⁴ m²

Therefore:

Q = (3.1416 × 10⁻⁴)(3)
Q = 9.425 × 10⁻⁴ m³/s

In litres per second:

Q = 0.9425 L/s
Final Answer for Q4(c): Nozzle diameter is approximately 1.10 cm, and water leaves the nozzle at 9.42×10⁻⁴ m³/s, or about 0.943 L/s.

Question 5: Double Slit, Grating Resolving Power and SHM

Full Question

Q.5. (a) Discuss analytical treatment of interference of light to calculate intensity in double slit interference. Describe the conditions of maximum and minimum intensity and also draw the intensity pattern for double slit interference.

Q.5. (b) What is resolving power of a grating? Show that it increases with the order of image.

Q.5. (c) A body having SHM has an amplitude of 5 cm and a period of 0.2 s. When the displacement is 5 cm, find the acceleration and velocity.

Q5(a): Analytical Treatment of Double Slit Interference

In Young’s double slit experiment, two coherent waves from two slits superpose on a screen and produce interference fringes. Let the intensities due to the two slits be I1 and I2, and the phase difference between them be δ.

The resultant intensity is:

I = I1 + I2 + 2√(I1I2)cosδ

If both slits have equal intensity:

I1 = I2 = I0

Then:

I = I0 + I0 + 2I0cosδ
I = 2I0(1+cosδ)

Using identity:

1 + cosδ = 2cos²(δ/2)

Therefore:

I = 4I0cos²(δ/2)

Phase Difference and Path Difference

If the path difference is Δ, phase difference is:

δ = 2πΔ/λ

For double slit:

Δ = d sinθ

Condition for Maximum Intensity

Maximum intensity occurs when:

cos²(δ/2) = 1

This gives:

δ = 2mπ

or:

d sinθ = mλ

At maximum:

Imax = 4I0

Condition for Minimum Intensity

Minimum intensity occurs when:

cos²(δ/2) = 0

This gives:

δ = (2m+1)π

or:

d sinθ = (m + 1/2)λ

At minimum:

Imin = 0

Intensity Pattern

Intensity
^
4I0| /\ /\ /\ /\ /\
| / \ / \ / \ / \ / \
|____/____\__/____\__/____\__/____\__/____\____> position
dark bright dark bright dark bright dark

Bright: d sinθ = mλ
Dark: d sinθ = (m+1/2)λ

Final Answer for Q5(a): For equal slit intensities, I=4I0cos²(δ/2). Maxima occur at d sinθ=mλ, and minima occur at d sinθ=(m+1/2)λ.

Q5(b): Resolving Power of a Grating

Resolving power of a grating is the ability to separate two close wavelengths. It is defined as:

R = λ/Δλ

For a diffraction grating:

R = mN

where:

  • m is order of spectrum.
  • N is number of illuminated grating lines.

Derivation

The grating equation is:

d sinθ = mλ

For a grating with N slits, the sharpness of principal maxima increases with the number of illuminated slits. Rayleigh’s criterion gives:

R = λ/Δλ = mN

This shows directly that resolving power is proportional to order m. If the order is increased, the resolving power increases.

R ∝ m
Final Answer for Q5(b): Resolving power of a grating is R=λ/Δλ=mN. It increases with the order of spectrum because R is directly proportional to m.

Q5(c): SHM Acceleration and Velocity

Given:

Amplitude, A = 5 cm = 0.05 m
Period, T = 0.2 s
Displacement, x = 5 cm = 0.05 m

Angular frequency is:

ω = 2π/T
ω = 2π/0.2
ω = 31.416 s⁻¹

Velocity

Velocity in SHM is:

v = ω√(A² – x²)

Here, x=A, so:

v = ω√(A² – A²)
v = 0

Acceleration

Acceleration in SHM is:

a = -ω²x

Substitute values:

a = -(31.416)²(0.05)
a = -49.35 m/s²

The negative sign means acceleration is directed toward the mean position.

Final Answer for Q5(c): At displacement 5 cm, the body is at the extreme position. Velocity is 0, and acceleration is -49.35 m/s² toward the mean position.

Question 6: Carnot Cycle, Gibbs Function and Heat Engine Efficiency

Full Question

Q.6. (a) What is Carnot Cycle? Draw and explain it for a reversible process.

Q.6. (b) What does Gibbs function describe? Prove that Gibbs function for a reversible isothermal and isobaric process is constant.

Q.6. (c) A heat engine absorbs 52.4 kJ of heat and exhausts 36.2 kJ of heat in each cycle. Calculate efficiency of heat engine and work done by engine per cycle.

Q6(a): Carnot Cycle

The Carnot cycle is an ideal reversible heat-engine cycle operating between two heat reservoirs. It consists of two reversible isothermal processes and two reversible adiabatic processes. It gives the maximum possible efficiency for any heat engine working between the same two temperatures.

Four Steps of Carnot Cycle

  1. Isothermal expansion at high temperature TH: Gas absorbs heat QH from the hot reservoir and does work.
  2. Adiabatic expansion: Gas expands without heat exchange, and its temperature falls from TH to TC.
  3. Isothermal compression at low temperature TC: Gas rejects heat QC to the cold reservoir.
  4. Adiabatic compression: Gas is compressed without heat exchange, and its temperature rises from TC back to TH.

Carnot Cycle Diagram

P
^
| A ─────── B Isothermal expansion at TH
| / \
| / \ Adiabatic expansion
| D ─────────── C Isothermal compression at TC
| Adiabatic compression
+——————————–> V

Carnot Efficiency

The efficiency of a Carnot engine is:

η = 1 – TC/TH

where temperatures must be in kelvin.

Final Answer for Q6(a): Carnot cycle is a reversible ideal cycle with two isothermal and two adiabatic processes. Its efficiency is η=1-TC/TH.

Q6(b): Gibbs Function

Gibbs free energy is a thermodynamic potential defined as:

G = H – TS

Since:

H = U + PV

we can write:

G = U + PV – TS

Gibbs function is especially useful for processes at constant temperature and constant pressure. It tells whether a process is spontaneous under these conditions.

Proof That Gibbs Function Is Constant for Reversible Isothermal and Isobaric Process

Start from:

G = U + PV – TS

Differentiate:

dG = dU + PdV + VdP – TdS – SdT

For a reversible process:

dU = TdS – PdV

Substitute into dG:

dG = (TdS – PdV) + PdV + VdP – TdS – SdT

Cancel terms:

TdS – TdS = 0
-PdV + PdV = 0

So:

dG = VdP – SdT

For an isothermal process:

dT = 0

For an isobaric process:

dP = 0

Therefore:

dG = V(0) – S(0) = 0

Hence:

G = constant
Final Answer for Q6(b): Gibbs function describes useful thermodynamic potential at constant temperature and pressure. For a reversible isothermal and isobaric process, dG=VdP-SdT=0, so Gibbs function is constant.

Q6(c): Heat Engine Efficiency and Work Done

Given:

Heat absorbed, QH = 52.4 kJ
Heat exhausted, QC = 36.2 kJ

Work done per cycle is:

W = QH – QC
W = 52.4 – 36.2
W = 16.2 kJ

Efficiency is:

η = W/QH
η = 16.2/52.4
η = 0.309

In percentage:

η = 30.9%
Final Answer for Q6(c): Work done by the engine per cycle is 16.2 kJ, and efficiency is approximately 30.9%.

Question 7: Clausius-Clapeyron, Adiabatic Relation and Isothermal Work

Full Question

Q.7. (a) Derive Clausius-Clapeyron equation and also write its two conclusions.

Q.7. (b) Prove that TV^(γ-1)=constant.

Q.7. (c) Air occupying 0.142 m³ at 2.04×10⁵ Pa is expanded isothermally to 1 atm and then cooled at constant pressure until it reaches its initial volume. Find work done on the gas.

Q7(a): Clausius-Clapeyron Equation

The Clausius-Clapeyron equation gives the slope of a phase boundary between two phases in a pressure-temperature diagram. It relates pressure, temperature, latent heat and change in volume during phase transition.

For two phases in equilibrium, Gibbs free energies are equal. Along the phase boundary:

dG1 = dG2

For one mole:

dG = VdP – SdT

Thus:

V1dP – S1dT = V2dP – S2dT

Rearrange:

(V2 – V1)dP = (S2 – S1)dT

Therefore:

dP/dT = (S2 – S1)/(V2 – V1)

During phase transition, entropy change is:

S2 – S1 = L/T

where L is latent heat per mole. Substitute:

dP/dT = L/[T(V2 – V1)]
Clapeyron Equation: dP/dT = L/[T(V2-V1)].

Clausius-Clapeyron Approximation for Vaporization

For vaporization, vapour volume is much greater than liquid volume:

Vvapour >> Vliquid

So:

V2 – V1 ≈ Vvapour

For ideal gas vapour:

V = RT/P

Substitute into Clapeyron equation:

dP/dT = LP/(RT²)

Rearrange:

dP/P = (L/R)(dT/T²)

Integrate:

lnP = -L/(RT) + constant

Two Conclusions

  1. Vapour pressure increases rapidly with temperature: The equation lnP=-L/(RT)+constant shows that vapour pressure rises strongly as temperature increases.
  2. Boiling point depends on external pressure: Lower external pressure lowers boiling point, while higher pressure raises boiling point. This explains boiling at lower temperature on mountains and higher temperature in pressure cookers.
Final Answer for Q7(a): Clausius-Clapeyron equation is dP/dT=L/[T(V2-V1)]. For vaporization, lnP=-L/(RT)+constant.

Q7(b): Proof of TV^(γ-1)=constant

For a reversible adiabatic process:

PV^γ = constant

Using ideal gas equation:

PV = nRT

So:

P = nRT/V

Substitute into adiabatic equation:

(nRT/V)V^γ = constant

Simplify:

nRT V^(γ-1) = constant

Since n and R are constants for a fixed amount of gas:

T V^(γ-1) = constant
Final Answer for Q7(b): For a reversible adiabatic process of an ideal gas, TV^(γ-1)=constant.

Q7(c): Work Done on Gas in Two-Step Process

Assumption: The pressure in the scan is interpreted as 2.04×10⁵ Pa. Final pressure after isothermal expansion is taken as 1 atm = 1.013×10⁵ Pa.

Given:

Initial volume, V1 = 0.142 m³
Initial pressure, P1 = 2.04×10⁵ Pa
Final pressure after isothermal expansion, P2 = 1.013×10⁵ Pa

Step 1: Find Volume After Isothermal Expansion

For isothermal expansion:

P1V1 = P2V2

Therefore:

V2 = P1V1/P2
V2 = (2.04×10⁵)(0.142)/(1.013×10⁵)
V2 ≈ 0.286 m³

Step 2: Work Done by Gas During Isothermal Expansion

For isothermal expansion:

W1 = P1V1 ln(V2/V1)

Since V2/V1 = P1/P2:

W1 = P1V1 ln(P1/P2)

Substitute values:

W1 = (2.04×10⁵)(0.142) ln[(2.04×10⁵)/(1.013×10⁵)]
W1 ≈ 2.03×10⁴ J

Step 3: Work During Constant-Pressure Cooling Back to Initial Volume

During constant-pressure cooling at P2, the gas volume decreases from V2 to V1.

W2 = P2(V1 – V2)
W2 = (1.013×10⁵)(0.142 – 0.286)
W2 ≈ -1.46×10⁴ J

Step 4: Net Work by Gas

Wby = W1 + W2
Wby = 2.03×10⁴ – 1.46×10⁴
Wby ≈ 5.7×10³ J

Step 5: Work Done on Gas

Work done on gas is the negative of work done by gas:

Won = -Wby
Won ≈ -5.7×10³ J
Final Answer for Q7(c): Net work done by the gas is approximately +5.7 kJ. Therefore, work done on the gas is approximately -5.7 kJ.

Question 8: Newton’s Rings, Polarization by Reflection and Doppler Effect

Full Question

Q.8. Write comprehensive notes on any two of the following:

(a) Newton’s rings

(b) Polarization by reflection

(c) Doppler effect

Exam Strategy: The paper asks for any two notes, but all three are solved below so students can choose the two they understand best.

Q8(a): Newton’s Rings

Newton’s rings are circular interference fringes formed due to interference of light reflected from the upper and lower surfaces of a thin air film between a plano-convex lens and a plane glass plate.

Formation

When a plano-convex lens is placed on a glass plate, a thin air film of varying thickness is formed between the two surfaces. The thickness is zero at the point of contact and increases outward. When monochromatic light falls normally, reflected rays from the upper and lower surfaces of the air film interfere and form circular bright and dark rings.

Why Rings Are Circular

The air film has the same thickness at all points located at the same distance from the point of contact. Therefore, the fringes are circular.

Condition for Dark Rings in Reflected Light

For reflected light, one ray undergoes a phase reversal of π. Therefore, the condition for dark rings is:

2t = mλ

For a plano-convex lens of radius of curvature R:

t = r²/(2R)

Substitute:

2(r²/2R) = mλ
r² = mλR

Diameter D=2r, so:

D_m² = 4mλR

Condition for Bright Rings in Reflected Light

2t = (m + 1/2)λ

Uses of Newton’s Rings

  1. Determination of wavelength of monochromatic light.
  2. Measurement of radius of curvature of a lens.
  3. Testing flatness of optical surfaces.
  4. Determination of refractive index of a liquid.
Note Summary: Newton’s rings are circular interference fringes formed by a thin air film. For dark rings in reflected light, D_m²=4mλR.

Q8(b): Polarization by Reflection

Polarization is the phenomenon in which vibrations of light are restricted to one plane. Since light is a transverse electromagnetic wave, it can be polarized.

When unpolarized light is reflected from a transparent dielectric surface such as glass or water, the reflected light becomes partially polarized. At a particular angle of incidence, called Brewster angle, the reflected light becomes completely plane-polarized.

Brewster’s Law

Brewster’s law states that the tangent of the polarizing angle is equal to the refractive index of the second medium relative to the first medium.

tanθB = n2/n1

If light travels from air into glass, then:

tanθB = n

where n is the refractive index of glass.

Relation Between Reflected and Refracted Rays

At Brewster angle, the reflected and refracted rays are perpendicular to each other.

θB + r = 90°

Explanation

At Brewster angle, the component of the electric field parallel to the plane of incidence is not reflected. The reflected beam therefore contains vibrations mainly perpendicular to the plane of incidence and becomes plane-polarized.

Applications

  1. Polarizing sunglasses reduce glare from roads and water surfaces.
  2. Photography filters remove unwanted reflections.
  3. Optical instruments use polarization control.
  4. Polarization helps study stress patterns and material properties.
Note Summary: Polarization by reflection occurs when reflected light becomes plane-polarized at Brewster angle. Brewster’s law is tanθB=n2/n1.

Q8(c): Doppler Effect

The Doppler effect is the apparent change in frequency or wavelength of a wave due to relative motion between the source and the observer.

If the source and observer move closer, the observed frequency increases. If they move away from each other, the observed frequency decreases.

Doppler Effect for Sound

For sound waves, the general formula is:

f’ = f[(v ± vo)/(v ∓ vs)]

Here:

  • f' is observed frequency.
  • f is source frequency.
  • v is speed of sound.
  • vo is speed of observer.
  • vs is speed of source.

Sign Convention

  1. If observer moves toward source, use v+vo.
  2. If observer moves away from source, use v-vo.
  3. If source moves toward observer, use v-vs.
  4. If source moves away from observer, use v+vs.

Examples

  1. The pitch of an ambulance siren increases as it approaches and decreases as it moves away.
  2. Police radar uses Doppler shift to measure vehicle speed.
  3. Astronomy uses red shift and blue shift to study motion of stars and galaxies.
  4. Medical Doppler ultrasound measures blood flow.

Doppler Effect for Light

For light, the Doppler effect appears as red shift or blue shift. If a source moves away, wavelength increases and light shifts toward red. If a source moves closer, wavelength decreases and light shifts toward blue.

Note Summary: Doppler effect is the apparent change in frequency due to relative motion between source and observer. It is used in sirens, radar, astronomy and medical ultrasound.

Revision Plan for CSS Physics Paper-I 2025 Solved

After reading this complete CSS Physics Paper-I 2025 Solved guide, revise it in three rounds. In the first round, learn the definitions and formulas. In the second round, reproduce the derivations without looking. In the third round, solve the numerical questions again with units and compare your final answer with the given result.

Question Revision Task
Q2 Prove Stokes theorem, show ∮∇φ·dl=0, and solve velocity/acceleration components again.
Q3 Compare the three statistics and recalculate pressure rise after paddle-wheel work.
Q4 Revise viscosity, explain water/mercury capillary behaviour and solve nozzle continuity.
Q5 Derive double slit intensity, prove R=mN and solve SHM acceleration/velocity.
Q6 Draw Carnot cycle, prove dG=0 at constant T and P, and solve heat-engine efficiency.
Q7 Derive Clausius-Clapeyron equation, prove adiabatic relation and solve two-step work problem.
Q8 Prepare any two notes but revise all three for safety: Newton’s rings, polarization and Doppler effect.

Related Resources for CSS Physics Paper-I 2025 Solved

Exam Note: Some scanned FPSC papers distort mathematical symbols. Where a symbol is unclear, state your assumption briefly, solve the standard Physics expression, keep units visible and write the final result clearly.

FAQs About CSS Physics Paper-I 2025 Solved

What does CSS Physics Paper-I 2025 Solved include?

CSS Physics Paper-I 2025 Solved includes complete solved answers for Q2 to Q8 with definitions, derivations, numerical calculations, formulas, final answers and exam-ready notes.

What is Stokes theorem?

Stokes theorem states that ∮C A·dl = ∬S (∇×A)·n dS. It relates circulation around a closed curve to the curl of the vector field over the surface bounded by the curve.

What are the velocity and acceleration components in Q2?

Using the interpreted curve, at t=1, v=4i-2j+3k and a=4i+2j. Components along 2i-3j+2k are 20/√17 ≈ 4.85 m/s and 2/√17 ≈ 0.485 m/s².

What is the pressure after paddle-wheel work in Q3?

The pressure rise is about 376.8 Pa, so the final pressure is approximately 101.7 kPa.

What is the nozzle diameter answer in Q4?

The required nozzle diameter is approximately 1.10 cm, and the flow rate is 9.42×10⁻⁴ m³/s.

What are the SHM velocity and acceleration answers in Q5?

At displacement equal to amplitude, velocity is 0, and acceleration is -49.35 m/s² toward the mean position.

What is the heat engine efficiency in Q6?

The engine absorbs 52.4 kJ and rejects 36.2 kJ. Work is 16.2 kJ, and efficiency is approximately 30.9%.

What is the net work answer in Q7?

The net work done by the gas is approximately +5.7 kJ. Therefore, work done on the gas is approximately -5.7 kJ.

Can I paste this HTML into WordPress?

Yes. The post avoids an H1 heading so your WordPress post title can remain the only H1. The internal structure begins with H2 and continues with H3/H4 headings.

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