Maharashtra State Board HSC Physics (54)
Date: 16 Feb 2026 | Max Marks: 70
SECTION - A
Q. 1. Multiple Choice Questions [10 Marks]
- (a) decreases
- (b) becomes zero
- (c) remains same
- (d) increases
- (a) only kinetic energy
- (b) both kinetic energy and potential energy
- (c) only potential energy
- (d) neither kinetic energy nor potential energy
- (a) decreases
- (b) becomes zero
- (c) remains same
- (d) increases
- (a) isobaric
- (b) isochoric
- (c) isothermal
- (d) adiabatic
- (a) \( 2\pi\sqrt{\frac{l\cos \theta}{g}} \)
- (b) \( 4\pi\sqrt{\frac{l\cos \theta}{4g}} \)
- (c) \( 2\pi\sqrt{\frac{l\sin \theta}{g}} \)
- (d) \( 4\pi\sqrt{\frac{l\tan \theta}{g}} \)
- (a) \( \frac{1}{2}B\omega l^{2} \)
- (b) \( B\omega l^{2} \)
- (c) \( 2B\omega l^{2} \)
- (d) \( B\omega l \)
- (a) 1:4
- (b) 1:2
- (c) 2:1
- (d) 4:1
\( \frac{\lambda_1}{\lambda_2} = \frac{E_2}{E_1} = \frac{2.5}{5} = \frac{1}{2} \).
- (a) 0
- (b) \( 2\sqrt{3} \)
- (c) 4
- (d) 12
\( R = \sqrt{2^2 + 2^2 + 2(2)(2)\cos(60^\circ)} = \sqrt{4+4+4} = \sqrt{12} = 2\sqrt{3} \).
- (a) 2 cm
- (b) 4 cm
- (c) 6 cm
- (d) 8 cm
\( L = \frac{m_{net}}{M_z \cdot A} = \frac{10}{10^6 \cdot 2.5 \times 10^{-4}} = \frac{10}{2.5 \times 10^2} = \frac{10}{250} = 0.04m = 4cm \).
- (a) negative
- (b) zero
- (c) positive
- (d) infinity
Q. 2. Answer the following questions [8 Marks]
For a point inside the shell (r < R): \( E = 0 \)
Since \( I \propto A^2 \), \( \frac{A_1}{A_2} = \sqrt{\frac{I_1}{I_2}} = \sqrt{\frac{25}{1}} = \frac{5}{1} \).
Ratio of amplitudes is 5:1.
\( p \rightarrow n + e^+ + \nu \)
Let \( T_1 = T \). Then \( T_2 = T + 0.21T = 1.21T \).
\( \frac{n_1}{n_2} = \sqrt{\frac{T_1}{T_2}} = \sqrt{\frac{T}{1.21T}} = \frac{1}{1.1} = \frac{10}{11} \).
Ratio \( n_1:n_2 = 10:11 \).
SECTION - B
Attempt any EIGHT questions [16 Marks]
Applications:
- Dead beat galvanometer: To stop the oscillation of the coil quickly.
- Induction Furnace: Used to melt metals using heat produced by eddy currents.
- Electric Brakes: Used in trains.
- Contact resistance at the points where wire is connected to copper strips.
- Non-uniformity of the bridge wire radius.
- Ends of the wire may not coincide exactly with the 0 and 100 cm marks of the scale (End error).
- Errors are minimized by obtaining the null point near the center of the wire (between 34cm and 66cm).
- By interchanging the positions of the unknown resistance and resistance box and taking the average.
(Note: In an exam, draw a diagram showing a slit S, the biprism, two virtual sources S1 and S2 created by refraction, and the overlapping region on the screen/eyepiece forming interference bands.)
1. Centripetal force = Electrostatic force: \( \frac{mv^2}{r} = \frac{1}{4\pi\epsilon_0}\frac{Ze^2}{r^2} \Rightarrow mv^2r = \frac{Ze^2}{4\pi\epsilon_0} \) ...(i)
2. Bohr's quantization condition: \( mvr = \frac{nh}{2\pi} \Rightarrow v = \frac{nh}{2\pi mr} \) ...(ii)
Substitute (ii) into (i): \( m(\frac{nh}{2\pi mr})^2 r = \frac{Ze^2}{4\pi\epsilon_0} \)
\( \frac{n^2 h^2}{4\pi^2 m r} = \frac{Ze^2}{4\pi\epsilon_0} \)
\( r = \frac{\epsilon_0 n^2 h^2}{\pi m Z e^2} \)
\( I = 2 kg m^2 \)
\( n = 60 rpm = 1 rps \Rightarrow \omega_f = 2\pi n = 2\pi rad/s \)
\( \omega_i = 0 \)
\( t = 2\pi s \)
Angular acceleration \( \alpha = \frac{\omega_f - \omega_i}{t} = \frac{2\pi - 0}{2\pi} = 1 rad/s^2 \)
Torque \( \tau = I\alpha = 2 \times 1 = 2 Nm \)
Power \( P = \tau \omega_f = 2 \times 2\pi = 4\pi \) Watts (approx 12.56 W).
\( q = 2\times 10^{-6} C \), \( 2l = 4 cm = 0.04 m \), \( E = 10^5 N/C \)
Dipole moment \( p = q \times 2l = 2\times 10^{-6} \times 0.04 = 8 \times 10^{-8} Cm \)
Work done \( W = pE(\cos\theta_1 - \cos\theta_2) \)
Assuming initial position is stable equilibrium (\(0^\circ\)) and turned to \(180^\circ\).
\( W = 8 \times 10^{-8} \times 10^5 (\cos 0^\circ - \cos 180^\circ) \)
\( W = 8 \times 10^{-3} (1 - (-1)) = 8 \times 10^{-3} (2) = 16 \times 10^{-3} J = 0.016 J \).
For a circular arc, the angle between current element \(dl\) and radius vector \(r\) is always \(90^\circ\) (\(\sin 90 = 1\)).
\( B = \int dB = \frac{\mu_0 I}{4\pi r^2} \int dl \).
\( \int dl \) is the length of the arc \( s = r\theta \).
\( B = \frac{\mu_0 I}{4\pi r^2} (r\theta) = \frac{\mu_0 I}{4\pi r} \theta \).
Advantages:
- Quick response (very fast switching speed).
- Linear response (Photocurrent is directly proportional to incident light intensity).
- Compact size and low cost.
- Its properties are temperature dependent (dark current increases with temperature).
- Active area is small, so it requires optical lenses to focus light.
- Requires external reverse bias voltage.
| Harmonics | Overtones |
|---|---|
| Harmonics are integral multiples of the fundamental frequency (n, 2n, 3n...). | Overtones are the actual frequencies present in the vibration above the fundamental frequency. |
| All harmonics may or may not be present in a given sound note. | Overtones are only those frequencies that are actually generated by the instrument. |
| The fundamental frequency is called the first harmonic. | The first frequency higher than the fundamental is called the first overtone. |
Given:
\( r = 0.3 \text{ mm} = 0.3 \times 10^{-3} \text{ m} = 3 \times 10^{-4} \text{ m} \)
\( v = 2 \text{ m/s} \)
\( \eta = 0.833 \text{ Ns/m}^2 \)
Formula: Stokes' Law
\( F = 6\pi \eta r v \)
Calculation:
\( F = 6 \times 3.142 \times 0.833 \times 3 \times 10^{-4} \times 2 \)
\( F = (6 \times 2 \times 3) \times 3.142 \times 0.833 \times 10^{-4} \)
\( F = 36 \times 3.142 \times 0.833 \times 10^{-4} \)
\( F \approx 94.22 \times 10^{-4} \text{ N} \)
Answer: The viscous force is \( 9.42 \times 10^{-3} \text{ N} \).
Condition: KE of gas molecule = Energy of electron
\( \frac{3}{2} k_B T = eV \)
\( T = \frac{2eV}{3k_B} \)
Calculation:
\( T = \frac{2 \times 1.6 \times 10^{-19} \times 1}{3 \times 1.4 \times 10^{-23}} \)
\( T = \frac{3.2}{4.2} \times 10^{4} \)
\( T = 0.7619 \times 10000 \)
\( T = 7619 \text{ K} \)
Inductance (\(L\)) = \( 200 \text{ mH} = 200 \times 10^{-3} \text{ H} = 0.2 \text{ H} \)
Peak e.m.f. (\(E_0\)) = \( 220 \text{ V} \)
Frequency (\(f\)) = \( 50 \text{ Hz} \)
To Find:
Peak current (\(I_0\)) = ?
Formulae:
1. Inductive Reactance: \( X_L = 2\pi f L \)
2. Peak Current: \( I_0 = \frac{E_0}{X_L} \)
Calculation:
First, calculate the Inductive Reactance (\(X_L\)):
\( X_L = 2 \times 3.142 \times 50 \times 0.2 \)
\( X_L = 3.142 \times 100 \times 0.2 \)
\( X_L = 3.142 \times 20 \)
\( X_L = 62.84 \, \Omega \)
Now, calculate the Peak Current (\(I_0\)):
\( I_0 = \frac{220}{62.84} \)
Using log tables (as per exam instructions):
\( \log(220) = 2.3424 \)
\( \log(62.84) = 1.7982 \)
Subtracting logs: \( 2.3424 - 1.7982 = 0.5442 \)
Antilog(0.5442) \( \approx 3.501 \)
Alternatively, by direct division:
\( I_0 \approx 3.501 \text{ A} \)
Answer:
The peak current in the circuit is 3.501 A.
SECTION - C
Attempt any EIGHT questions [24 Marks]
(a) Mechanical Equilibrium: When there are no unbalanced forces within the system and between the system and its surroundings (Pressure is constant).
(b) Chemical Equilibrium: When the chemical composition of the system does not change with time (No chemical reactions).
(c) Thermal Equilibrium: When the temperature of the system is uniform throughout and does not change with time.
\( Z = \sqrt{R^2 + (X_L - X_C)^2} \). For Z to be minimum, \( X_L = X_C \).
\( \omega L = \frac{1}{\omega C} \Rightarrow \omega^2 = \frac{1}{LC} \)
\( \omega = \frac{1}{\sqrt{LC}} \)
Since \( \omega = 2\pi f_r \), \( 2\pi f_r = \frac{1}{\sqrt{LC}} \)
\( f_r = \frac{1}{2\pi\sqrt{LC}} \)
Magnetization (Mz): The net magnetic dipole moment per unit volume. \( M_z = \frac{m_{net}}{V} \).
SI Unit: Ampere/meter (A/m).
Dimensions: \( [L^{-1} M^0 T^0 I^1] \).
Relation: \( \mu = \mu_0 (1 + \chi) \) where \(\chi\) is susceptibility.
Consider a point charge \( +q \) placed at origin \( O \). We want to determine the electric potential at a point \( P \) at a distance \( r \) from \( O \).
1. Definition: Electric potential at a point is the work done in bringing a unit positive charge from infinity to that point against the electrostatic force.
2. Force at intermediate point: Consider an intermediate point \( M \) at a distance \( x \) from \( O \) on the path from infinity to \( P \). The electrostatic force on a unit positive charge at \( M \) is:
$$ F = \frac{1}{4\pi\epsilon_0} \frac{q \times 1}{x^2} $$ (Directed away from the charge).
3. Work done for small displacement: The work done \( dW \) to move the unit charge against this force through a small distance \( dx \) (towards \( O \)) is:
$$ dW = -F dx $$ (Negative sign indicates work is done against the repulsive force).
4. Total Work Done: Total work done in moving the unit charge from \( \infty \) to \( r \) is obtained by integrating \( dW \):
$$ W = \int_{\infty}^{r} - \left( \frac{1}{4\pi\epsilon_0} \frac{q}{x^2} \right) dx $$
$$ W = - \frac{q}{4\pi\epsilon_0} \int_{\infty}^{r} x^{-2} dx $$
Using \( \int x^n dx = \frac{x^{n+1}}{n+1} \):
$$ W = - \frac{q}{4\pi\epsilon_0} \left[ \frac{x^{-1}}{-1} \right]_{\infty}^{r} $$
$$ W = \frac{q}{4\pi\epsilon_0} \left[ \frac{1}{x} \right]_{\infty}^{r} $$
$$ W = \frac{q}{4\pi\epsilon_0} \left( \frac{1}{r} - \frac{1}{\infty} \right) $$
$$ W = \frac{1}{4\pi\epsilon_0} \frac{q}{r} $$
5. Conclusion: By definition, this work done is the electrostatic potential \( V \).
$$ V = \frac{1}{4\pi\epsilon_0} \frac{q}{r} $$
Consider an electron with mass \( m \) and charge \( e \) accelerated from rest through a potential difference \( V \).
1. Kinetic Energy: The work done on the electron by the electric field appears as its kinetic energy (\( E_k \)).
$$ E_k = eV $$ ...(i)
2. Momentum relation: If \( v \) is the velocity of the electron, then \( E_k = \frac{1}{2}mv^2 \). Multiplying and dividing by \( m \):
$$ E_k = \frac{m^2v^2}{2m} = \frac{p^2}{2m} $$
Where \( p = mv \) is the momentum. Thus:
$$ p = \sqrt{2mE_k} $$ ...(ii)
3. de-Broglie Wavelength: According to de-Broglie's hypothesis, the wavelength \( \lambda \) associated with a material particle of momentum \( p \) is:
$$ \lambda = \frac{h}{p} $$
Substituting value of \( p \) from (ii):
$$ \lambda = \frac{h}{\sqrt{2mE_k}} $$
Substituting \( E_k = eV \) from (i):
$$ \lambda = \frac{h}{\sqrt{2meV}} $$
4. Standard Calculation (Optional but recommended): Substituting standard values: \( h = 6.63 \times 10^{-34} Js \) \( m = 9.1 \times 10^{-31} kg \) \( e = 1.6 \times 10^{-19} C \)
$$ \lambda = \frac{1.228}{\sqrt{V}} \text{ nm} $$
The circuit consists of a center-tapped transformer, two diodes (\(D_1\) and \(D_2\)), and a load resistor (\(R_L\)).
2. Working:
- Positive Half Cycle: During the positive half cycle of the AC input, terminal A of the secondary coil becomes positive with respect to the center tap (C), and terminal B becomes negative.
- Diode \(D_1\) is forward biased and conducts current.
- Diode \(D_2\) is reverse biased and does not conduct.
- Current flows through \(R_L\) from X to Y.
- Negative Half Cycle: During the negative half cycle of the AC input, terminal A becomes negative with respect to C, and terminal B becomes positive.
- Diode \(D_1\) is reverse biased and does not conduct.
- Diode \(D_2\) is forward biased and conducts current.
- Current again flows through \(R_L\) from X to Y (same direction).
3. Conclusion: Since current flows through the load resistor in the same direction during both half cycles of the input AC voltage, the output is unidirectional (DC). This process is called full wave rectification.
4. Input-Output Waveforms:
[Image of input and output waveforms of full wave rectifier]
The output waveform shows pulsating DC voltage with a frequency twice that of the input AC frequency (Ripple frequency = \(2f\)).
According to the law of length, frequency is inversely proportional to vibrating length (\(n \propto \frac{1}{l}\)).
\( n_1 l_1 = n_2 l_2 \)
\( 112 \times 80 = 160 \times l_2 \)
\( l_2 = \frac{112 \times 80}{160} = \frac{112}{2} = 56 cm \).
The string should be pressed at 56 cm from the bridge (or the vibrating part should be 56 cm).
Isothermal Process (T constant).
\( W = nRT \ln(\frac{V_f}{V_i}) = 2.303 nRT \log_{10}(\frac{V_f}{V_i}) \)
\( W = 2.303 \times 0.5 \times 8.31 \times 300 \times \log(\frac{6}{2}) \)
\( W = 2.303 \times 0.5 \times 8.31 \times 300 \times 0.4771 \)
\( W \approx 1369.5 J \)
(b) For isothermal, \( \Delta U = 0 \), so \( Q = W = 1369.5 J \).
Given: \( G = 40\Omega, I_g = 4mA = 0.004 A \).
(a) Ammeter (0.4A): Connect Shunt (S) in parallel.
\( S = \frac{I_g G}{I - I_g} = \frac{0.004 \times 40}{0.4 - 0.004} = \frac{0.16}{0.396} \approx 0.404 \Omega \).
(b) Voltmeter (5V): Connect Resistance (X) in series.
\( X = \frac{V}{I_g} - G = \frac{5}{0.004} - 40 = 1250 - 40 = 1210 \Omega \).
Ampere's Law states: \( \oint \vec{B} \cdot d\vec{l} = \mu_0 I_{enclosed} \)
Case (i): For \( a < r < b \) (Inside the cable, between conductors)
Consider an Amperian loop of radius \( r \) such that \( a < r < b \).
The loop encloses only the current flowing through the inner conductor (radius \( a \)). Let this current be \( I \).
\( \oint B dl = B (2\pi r) \)
\( I_{enclosed} = I \)
Therefore, \( B (2\pi r) = \mu_0 I \)
Magnitude: \( B = \frac{\mu_0 I}{2\pi r} \)
Direction: Tangential to the circular loop (determined by Right Hand Thumb Rule).
Case (ii): For \( r > b \) (Outside the cable)
Consider an Amperian loop of radius \( r \) such that \( r > b \).
The loop encloses currents from both conductors:
- Inner conductor carries current \( +I \) (e.g., out of page).
- Outer conductor carries current \( -I \) (equal magnitude, opposite direction, e.g., into page).
Using Ampere's Law:
\( B (2\pi r) = \mu_0 (0) \)
\( B (2\pi r) = 0 \)
Magnitude: \( B = 0 \)
Direction: Not applicable (as field is zero).
\( E_n \propto \frac{1}{n^2} \).
\( E_2 = -3.4 eV \). Also \( E_2 = \frac{E_1}{2^2} \Rightarrow E_1 = 4 \times (-3.4) = -13.6 eV \).
Energy in 3rd orbit: \( E_3 = \frac{E_1}{3^2} = \frac{-13.6}{9} = -1.51 eV \).
Kinetic Energy (3rd): \( K.E. = |E_3| = 1.51 eV \).
Potential Energy (3rd): \( P.E. = 2 \times E_3 = 2 \times (-1.51) = -3.02 eV \).
SECTION - D
Attempt any THREE questions [12 Marks]
Work done by excess pressure = Increase in Surface Energy
\( (P_i - P_o) \cdot 4\pi r^2 \cdot \Delta r = T \cdot 2 \cdot (8\pi r \Delta r) \)
\( P_i - P_o = \frac{4T}{r} \).
Let \( Q \) be the total amount of radiant energy incident on the surface of a body.
When this radiation falls on the body, it is partly absorbed, partly reflected, and partly transmitted.
Let:
- \( Q_a \) = Amount of radiant energy absorbed.
- \( Q_r \) = Amount of radiant energy reflected.
- \( Q_t \) = Amount of radiant energy transmitted.
$$Q_a + Q_r + Q_t = Q$$
Dividing both sides by \( Q \):
$$\frac{Q_a}{Q} + \frac{Q_r}{Q} + \frac{Q_t}{Q} = \frac{Q}{Q}$$
$$\frac{Q_a}{Q} + \frac{Q_r}{Q} + \frac{Q_t}{Q} = 1$$
By definition:
- Coefficient of absorption \( a = \frac{Q_a}{Q} \)
- Coefficient of reflection \( r = \frac{Q_r}{Q} \)
- Coefficient of transmission \( t_r \) (or \( t \)) \( = \frac{Q_t}{Q} \)
$$a + r + t_r = 1$$
Conclusion: The sum of the coefficients of absorption, reflection, and transmission is always equal to unity (1).
Hydrogen (\(H_2\)):
Temperature \( T_1 = 127^\circ C = 127 + 273 = 400 K \)
Molecular Mass \( M_1 = 2 \)
Oxygen (\(O_2\)):
Temperature \( T_2 = 27^\circ C = 27 + 273 = 300 K \)
Molecular Mass \( M_2 = 32 \)
Formula:
Root Mean Square speed \( v_{rms} = \sqrt{\frac{3RT}{M}} \)
Since \( R \) is constant, \( v_{rms} \propto \sqrt{\frac{T}{M}} \)
Calculation:
Let \( v_1 \) be the r.m.s speed of Hydrogen and \( v_2 \) be the r.m.s speed of Oxygen.
$$\frac{v_1}{v_2} = \sqrt{\frac{T_1}{M_1} \times \frac{M_2}{T_2}}$$
$$\frac{v_1}{v_2} = \sqrt{\frac{400}{2} \times \frac{32}{300}}$$
$$\frac{v_1}{v_2} = \sqrt{200 \times \frac{32}{300}}$$
$$\frac{v_1}{v_2} = \sqrt{\frac{2 \times 32}{3}}$$
$$\frac{v_1}{v_2} = \sqrt{\frac{64}{3}}$$
$$\frac{v_1}{v_2} = \frac{8}{\sqrt{3}}$$
Answer:
The ratio of r.m.s speed of Hydrogen to Oxygen is \( 8 : \sqrt{3} \) (or approx \( 4.62 : 1 \)).
Area of loop (\(A\)) = \( 1 m^2 \)
Initial Magnetic Field (\(B_1\)) = \( 3 Wb/m^2 \)
Final Magnetic Field (\(B_2\)) = \( 1 Wb/m^2 \)
Time interval (\(dt\)) = \( 0.5 s \)
Formula:
According to Faraday's Law of Electromagnetic Induction:
$$ |e| = \left| \frac{d\phi}{dt} \right| = \left| \frac{d(BA)}{dt} \right| = A \left| \frac{dB}{dt} \right| $$
Calculation:
Change in Magnetic Field (\(dB\)) = \( B_2 - B_1 \)
\( dB = 1 - 3 = -2 Wb/m^2 \)
Magnitude of change \( |dB| = 2 Wb/m^2 \)
Substituting in the formula:
$$ |e| = 1 \times \frac{2}{0.5} $$
$$ |e| = \frac{2}{0.5} = 4 V $$
Answer:
The induced e.m.f. produced in the coil is 4 Volts.
Consider Young's double slit experiment setup:
- Let \( S_1 \) and \( S_2 \) be two coherent monochromatic sources separated by distance \( d \).
- Let \( D \) be the distance between the sources and the screen.
- Let \( \lambda \) be the wavelength of light.
- Consider a point \( P \) on the screen at a distance \( y \) (or \( x \)) from the central bright point \( O \).
1. Path Difference:
The path difference between the waves reaching \( P \) from \( S_1 \) and \( S_2 \) is:
$$ \Delta x = S_2P - S_1P $$
From geometry, for \( D >> d \), the path difference is approximated as:
$$ \Delta x = \frac{y d}{D} $$
2. Condition for Bright Fringes (Constructive Interference):
For a bright fringe at \( P \), the path difference must be an integral multiple of wavelength (\( n\lambda \)).
$$ \frac{y_n d}{D} = n\lambda $$
Where \( n = 0, 1, 2, ... \)
Therefore, the distance of the \( n^{th} \) bright fringe from the center is:
$$ y_n = \frac{n \lambda D}{d} $$
3. Expression for Fringe Width (\( X \)):
Fringe width is defined as the distance between two consecutive bright (or dark) fringes.
Let's find the distance between the \( n^{th} \) and \( (n+1)^{th} \) bright fringe.
Distance of \( (n+1)^{th} \) bright fringe:
$$ y_{n+1} = \frac{(n+1) \lambda D}{d} $$
Fringe Width \( X = y_{n+1} - y_n \)
$$ X = \frac{(n+1) \lambda D}{d} - \frac{n \lambda D}{d} $$
$$ X = \frac{\lambda D}{d} (n + 1 - n) $$
$$ X = \frac{\lambda D}{d} $$
Conclusion:
The expression for fringe width is \( X = \frac{\lambda D}{d} \).
It shows that fringe width is directly proportional to wavelength (\( \lambda \)) and distance of screen (\( D \)), and inversely proportional to slit separation (\( d \)).