marking scheme

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MARKING SCHEME
SET 55/1/A
Expected Answer / Value Points
Q. No.
Marks Total
Marks
Section - A
Set -1,Q1
Set- 2,Q5
Set-3, Q2
Set -1, Q2
Set- 2, Q4
Set-3, Q5
Set -1, Q3
Set- 2,Q2
Set-3, Q4
Set -1, Q4
Set- 2,Q3
Set-3, Q1.
Set -1, Q5
Set- 2,Q1
Set-3, Q3.
Dielectric Constant of a medium is the ratio of intensity of electric field in
free space to that in the dielectric medium.
Alternatively
It is the ratio of capacitance of a capacitor with dielectric medium to that
without dielectric medium.
Alternatively
Any other equivalent definition
S.I. Unit : No Unit
T1 > T2
Slope of T1 is higher than that of T2.
(or Resistance, at T1, is higher than that of T2)
No induced current hence no direction.
½
½
½
½
1
1
½ ,½
1
Critical angle depends upon the refractive index (n) of the medium ½ +½
and refractive index is different for different colours of light.
1
1
It rejects dc and sinusoids of frequency πœ”m, 2πœ”m and 2πœ”c and retain
frequencies πœ”c, πœ”c ± πœ”m.
(Alternatively: It allows only the desired/ required frequencies to pass
through it)
Section - B
Set -1, Q6
Set- 2,Q7
Set-3, Q10
Graph of V vs R
Graph of I vs R
1
1
(i) V vs R:
V
E
𝑉=
𝐸𝑅
𝑅+π‘Ÿ
1
R
I
(ii) I vs R:
𝐸/π‘Ÿ
𝐸
𝐼=
𝑅+π‘Ÿ
1
2
R
(Award ½ mark in each if child writes only formulae)
Ajmer SET I Page 1 of 15
Final Draft
17/3/2015
5:08 p.m.
Set -1, Q7
Set- 2,Q10
Set-3, Q8
de Broglie Relation
Dependence of πœ† on 𝑛
½
1
𝑕
de Broglie wavelength πœ† = π‘šπ‘£
1
½
1
½
1
∴ πœ† ∝𝑣 ; 𝑣 ∝𝑛
∴πœ†∝𝑛
∴ 𝑑𝑒 Broglie wavelength will increase
2
Alternative method
As 2πœ‹π‘Ÿπ‘› = π‘›πœ† ; λ =
π‘Ÿπ‘› ∝ 𝑛2
2πœ‹π‘Ÿπ‘›
𝑛
(πœ† ∝
π‘Ÿπ‘›
𝑛
)
1
½
𝑛2
∴ πœ† ∝ 𝑛 ⇒ πœ†∝𝑛
∴ 𝑑𝑒 Broglie wavelength will increase
½
2
(Note: Accept any other alternative method)
Set -1, Q8
Set- 2,Q6
Set-3, Q9
Definition of Wave front
Diagram
1
1
Wave front : It is the locus of points which oscillate in phase.
Or
It is a surface of constant phase.
1
1
2
Or
a) Characteristics & reason
b) Ratio of Velocity
½+½
1
a) Frequency does not change, as frequency is a characteristic of the source ½+½
of waves.
𝒗
𝒗
(Alternatively: π€πŸ = π€πŸ = 𝑛)
𝟏
𝟐
b) The ratio of velocities of wave in two media of refractive indices µ1 and µ2
1
µ
is µ 2 .
1
𝒗
(Alternatively: π’—πŸ =
𝟐
µπŸ
µπŸ
2
)
Ajmer SET I Page 2 of 15
Final Draft
17/3/2015
5:08 p.m.
Set -1, Q9
Set- 2,Q8
Set-3, Q7
Diagrams of AM and FM
Reason
1
1
½
½
Why FM is preferred over AMβ€Ÿ?
Low noise/ disturbance// reduced channel interference// more power can be 1
transmitted// high fidelity.
(Any one reason)
Set -1,Q10
Set- 2,Q9
Set-3, Q6
Formula
Calculation & result
Distance of the closest approach
1
π‘Ÿπ‘œ = 4πœ‹∈ βˆ™
0
=
2
½
1½
2𝑧𝑒 2
½
𝐸∝
2 × 9×10 9 ×80 ×(1.6 ×10 −19 )2
1
4.5 × 10 6 ×1.6 ×10 −19
= 5.12 × 10−14 π‘š
½
2
Section – C
Set -1,Q11
Set- 2,Q20
Set-3, Q15
Diagram
Force on each arm
Calculation of moment of couple
Orientation in stable equilibrium
Ajmer SET I Page 3 of 15
½
½
1
1
Final Draft
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½
Set -1,Q12
Set- 2,Q21
Set-3, Q16
Force on each perpendicular arm
𝐹1 = 𝐹2 = 𝐼 𝑏 𝐡
½
Moment of couple = 𝐼 𝑏 𝐡. π‘Ž sin πœƒ
𝜏 = 𝐼 π‘Žπ‘ 𝐡 π‘ π‘–π‘›πœƒ
𝜏 = I 𝐴𝐡 π‘ π‘–π‘›πœƒ 𝜏 = I 𝐴 × π΅
When the plane of the loop is perpendicular to the magnetic field, the loop
will be in stable equilibrium (𝐴 βˆ₯ 𝐡 ), ⟹ πœƒ = 0°
(If the student follows the following approach, award ½ marks only)
𝑀 = Equivalent magnetic moment of the planer loop = I𝐴
∴ Torque = 𝑀 × π΅ = I𝐴 × π΅
π‘‡π‘œπ‘Ÿπ‘žπ‘’π‘’ = IABπ‘ π‘–π‘›πœƒ
1
½
Production of em waves
Source of energy
Identification
1
1
½+½
Electromagnetic waves are produced by accelerated / oscillating charges
which produces oscillating electric field and magnetic field (which regenerate
each other).
Source of the Energy: Energy of the accelerated charge. (or the source that
accelerates the charges)
Identification:
(1) Infra red radiation
(2) X - rays
Set -1,Q13
Set- 2,Q22
Set-3, Q17
a) To draw path of light ray in prism
Formula and calculation of refractive index of liquid
b) Tracing the path of the ray
Ajmer SET I Page 4 of 15
3
½
1
1
½
½
3
½
1½
1
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a)
A
60°
B
60°
90°
½
C
𝑠𝑖𝑛𝑖𝑐 =
οƒ°
1
πœ‡π‘šπ‘”
=
πœ‡π‘š
πœ‡π‘”
½
πœ‡ π‘š = πœ‡π‘” 𝑠𝑖𝑛𝑖𝑐
½
½
3
=1.5 × 2 (𝑖𝑐 = 60°)
= 1.299 ≃ 1.3
(b)
1
3
Alternatively
Set -1,Q14
Set- 2,Q16
Set-3, Q18
Logic circuit –
Truth Table Identification -
1
1
1
To draw the logic circuit
A
1
B
Ajmer SET I Page 5 of 15
Final Draft
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Truth Table
A
0
1
0
1
B
0
0
1
1
Y
0
0
0
1
1
1
Identification : AND gate
3
Or
Identification of logic operation in circuit (a) & (b)
Truth table for circuit (a) & (b)
Identification of equivalent gates
½+½
½+½
½+½
½
½
Logic Operation a) Y = A.B
b) Y = A+B
Truth Table
a)
A
0
1
0
1
B
0
0
1
1
Y
0
0
0
1
A
0
1
0
1
B
0
0
1
1
Y
0
1
1
1
½
b)
½
Identification
a) AND gate
b) OR gate
Set -1,Q15
Set- 2,Q17
Set-3, Q11
Circuit diagram
Working
Wave forms and Input & Output
Characteristic property
Ajmer SET I Page 6 of 15
½
½
3
1
½
½+½
½
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Circuit Diagram
1
Description of Working- During the positive half of input ac diode D1 get forward bias
and D2, reverse biased and during negative half of input ac, polarity get reversed, D2 get
forward bias and D1 reverse bias. Hence, output is obtained across RL during entire cycle
of ac.
½
Wave forms
Input
½
Output
½
Characteristic property
Diode allows the current to pass only when it is forward based.
Set -1,Q16
Set- 2,Q18
Set-3, Q12
Set -1,Q17
Set- 2,Q19
Set-3, Q13
Explanation of (i), (ii) and (iii) with justification
Ajmer SET I Page 7 of 15
3
½+½
½+½
½+½
3
1×3
(i) Drift velocity will become half as 𝑣𝑑 ∝ 𝑉
1
(ii) Drift velocity will become half as 𝑣𝑑 ∝
𝐿
(iii) Drift velocity will remain the same as 𝑣𝑑 is independent of diameter (D).
Determination of magnetic field
Determination of kinetic energy in 𝑀𝑒𝑉
½
1½
1½
Final Draft
17/3/2015
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Magnetic field 𝐡 = 2πœ‹π‘šπ‘£/π‘ž
½
2 × 3.14 × 1.67 × 10−27 × 107
=
= 0.66𝑇
1.6 × 10−19
1
Final velocity of proton 𝑣 = 𝑅 × 2πœ‹π‘£ = 0.6 × 2 × 3.14 × 107
= 3.77 × 107 π‘š/𝑠
1
Energy = 2 π‘šπ“‹ 2 =
= 7.4 𝑀𝑒𝑉
Set -1,Q18
Set- 2,Q11
Set-3, Q14
1
2
½
× 1.67 × 10−27 × (3.77 × 107 )2 𝑗
a) Calculation of distance of third bright fringe
b) Calculation of distance from the central maxima
a) Distance of third bright fringe-𝑦3 =
=
½
½
1
2
π‘›πœ†π·
½
𝑑
3 × 520 × 10−9 × 1
1.5 × 10−3
½
= 1.04 × 10−3 π‘š ≃ 1 π‘šπ‘š
b) Let 𝑛𝑑𝑕 maxima of 650π‘›π‘š coincides with the (𝑛 + 1)𝑑𝑕 maxima of
520π‘›π‘š
∴ 𝑛 × 650 × 10−9 = 𝑛 + 1 520 × 10−9
⇒𝑛=4
∴ The least distance of the point is given by
π‘›π·πœ†1
𝑦=
𝑑
4 × 1 × 650 × 10−9
=
π‘š = 1.733 × 10−3 π‘š ≃ 1.7π‘šπ‘š
1.5 × 10−3
Set -1,Q19
Set- 2,Q12
Set-3, Q21
3
a) Pointing out and Reason of two processes
b) Identification of radioactive radiations
½
½
1
3
1+1
½+½
a) Nuclear fission of E to D and C; as there is a increase in binding ½ + ½
energy per nucleon
b) Nuclear fusion of A and B into C; as there is a increase in binding ½ + ½
energy per nucleon
b) First step - ∝ particle
Second step – 𝛽 particle
Ajmer SET I Page 8 of 15
½
½
Final Draft
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3
5:08 p.m.
Set -1,Q20
Set- 2,Q13
Set-3, Q22
Three modes of propagation
Brief explanation of reflection by Ionosphere
Effect of increased frequency range
1½
1
½
Three modes of propagation
i)
Ground Waves
ii)
Sky Waves
iii)
Space Waves
Set -1,Q21
Set- 2,Q14
Set-3, Q19
½
½
½
Ionosphere acts as a reflector for the range of frequencies from few MHz to
30 MHz . The ionospheric layers bend the radio waves back to the Earth.
1
Waves of frequencies greater than 30 MHz penetrate the ionosphere and
escape
½
Definition of Stopping Potential and threshold frequency
Determination using Einsteinβ€Ÿs Equation
3
1+1
1
Stopping Potential: The minimum negative potential applied to the anode/
plate for which photoelectric current become zero.
1
Threshold frequency: The minimum (cut off) frequency of incident radiation,
below which no emission of photoelectrons takes place.
1
By Einsteinβ€Ÿs Equation
𝑒𝑉0 = 𝑕𝑣 − Ο•o
For any given frequency 𝑣 > π‘£π‘œ , π‘‰π‘œ can be determined.
Stopping Potential 𝑉0 =
𝑕
𝑒
𝑣−
½
Ο•o
𝑒
as Ο•0 = 𝑕𝑣0
Threshold frequency,
Set -1,Q22
Set- 2,Q15
Set-3, Q20
𝑉0 =
½
πœ™0
𝑕
Calculation of voltage across each capacitor in (a), (b) and (c)
Explanation with reason for the change/no change
1½
1½
(a) V𝐿 = 3𝑉
V𝑅 = 3𝑉
(L: Left, R: Right)
(b) V𝐿 = 6𝑉
V𝑅 = 3𝑉
(c) V𝐿 = 2𝑉
V𝑅 = 3𝑉
Reasons
(a) No change – ( potential same on both capacitors as (V𝐿 = V𝑅 ))
(b) Charge on left hand capacitor will decrease ( V𝐿 > V𝑅 )
(c) Charge on left hand capacitor will increase ( V𝑅 > V𝐿 )
Ajmer SET I Page 9 of 15
3
Final Draft
½
½
½
½
½
½
17/3/2015
3
5:08 p.m.
Set -1,Q23
Set- 2,Q23
Set-3, Q23
(a) Naming the principle involved
(b) Explanation
(c) Two qualities
1
1
2
(a) Metal detector works on the principle of resonance in ac circuits.
1
(b) When a person walks through the gate of a metal detector, the impedance 1
of the circuit changes, resulting in significant change in current in the
circuit that causes a sound to be emitted as an alarm.
(c) Two qualities
(i) Following the rules/regulations
(ii) Responsible citizen
1+1
(iii) Scientific temperament
(iv) Knowledgable
(Any two)
4
Section - E
Set -1,Q24
Set- 2,Q26
Set-3, Q25
(a) Drawing labeled ray diagram
(b) Deducing relation between u , v and R
(c) Obtaining condition for real image
1½
2½
1
1½
From the diagram :
½
½
∠ 𝑖 = ∠𝑁𝑂𝑀 + ∠ 𝑁𝐢𝑀
∠ π‘Ÿ = ∠𝑁𝐢𝑀 − ∠ 𝑁𝐼𝑀
By Snellβ€Ÿs law ,
𝑛1 sin 𝑖 = 𝑛2 sin π‘Ÿ
½
Substituting for i and r. and simplifying, we get
𝑛1
𝑛2
𝑛2 − 𝑛1
+
=
𝑂𝑀 𝑀𝐼
𝑀𝐢
Substituting values of OM , MI and MC
𝑛2
𝑛1
𝑛 2 −𝑛 1
−
=
𝜐
𝑒
𝑅
Ajmer SET I Page 10 of 15
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½
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(b)Condition for real image : ν is positive
½
𝑛2
∴
>0
𝑣 𝑛
𝑛 −𝑛
From the derived relation , we have 𝑒1 < 2 𝑅 1
𝑛1 𝑅
∴ 𝑒 >
𝑛2 − 𝑛1
½
5
OR
(a) Ray diagram
Derivation of expression for magnifying power
(b) Effect on resolving power in each case; with justification
1½
1½
1+1
1½
(Award 1 mark if the student draws the diagram for image at distance of
distinct vision, deduct ½ mark for not showing the direction of Propogation of
ray)
Derivation:
-
Magnification due to objective
π‘šπ‘œ =
-
Magnification due to eyelens
π‘šπ‘’ =
-
𝐿
π‘“π‘œ
𝐷
𝑓𝑒
Total magnification π‘š = π‘šπ‘œ π‘šπ‘’
𝐿 𝐷
π‘šπ‘œ = .
π‘“π‘œ 𝑓𝑒
½
½
½
(b) The resolving power of microscope
1
(i) Will decrease with decrease of the diameter of objective lens as resolving
5
power is directly proportional to the diameter
Ajmer SET I Page 11 of 15
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(ii) Will decrease with increase of the wavelength of the incident light as 1
resolving power is inversely proportional to the wave length
Set -1,Q25
Set- 2,Q24
Set-3, Q26
(a) Faradayβ€Ÿs law
(b) Explanation with example
(c) Derivation for induced emf
1
2
2
(a) Faradayβ€Ÿs law – “The magnitude of the induced emf in a circuit is
equal to the time rate of change of magnetic flux through the circuit.”
(Alternatively : Induced emf =
−𝑑∅
𝑑𝑑
1
)
(b) A bar magnet experiences a repulsive force when brought near a
closed coil and attractive force when moved away from the coil, due
to induced current. Therefore, external work is required to be done in
the process.
(c) Since workdone is moving the charge „qβ€Ÿ across the length „lβ€Ÿ of the
conductor is
W=qvBl
Since emf is the work done per unit charge
w
β„°=
q
β„° = Blv
OR
(a) Derivation for the current using phasor diagram
1
Plot of graphs (i) and (ii)
(b) Derivation for the average power
1+1
2
2
1
1
5
Phasor diagram for the circuit:
½
From the Phasor diagram:
V makes an angle „ωtβ€Ÿ with axis, current „Iβ€Ÿ lags behind the voltage
πœ‹
πœ‹
„Vβ€Ÿ by 2 , (makes an angle of – ( 2 − 𝑀𝑑) with the axis.)
πœ‹
πœ‹
∴, 𝑖 = π‘–π‘š sin − 2 − πœ”π‘‘ = π‘–π‘š sin πœ”π‘‘ − 2
[Award this 1mark even if derivation is done by analytical method]
½
Ajmer SET I Page 12 of 15
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Graph showing variation of voltage and current as function of πœ”π‘‘
1+1
Instantaneous power in LCR circuit:
p=v×i
= vm sin ωt × im sin(ωt +φ)
𝑣 𝑖
p = π‘š2 π‘š [cos πœ‘ − cos 2πœ”π‘‘ + πœ‘ ]
average power Pav=
π‘£π‘š 𝑖 π‘š
Pav=
2
½
½
cos πœ‘
½
π‘£π‘š 𝑖 π‘š
cos πœ‘
2 2
𝑃 = 𝑉𝑒𝑓𝑓 𝐼𝑒𝑓𝑓 cos πœ™
Set -1,Q26
Set- 2,Q25
Set-3, Q24
½
a)Statement of Gauss law
Explanation with diagram
b)Magnitude and direction of net electric field in (i) and (ii)
(a)
5
1
1
1½ +1 ½
1
Gauss Law: Electric flux through a closed surface is πœ– times the total
0
charge enclosed by the surface.
1
Alternatively: πœ™ = πœ– . π‘ž
1
0
(a)The
+1 term q equals the sum of all charges enclosed by the surface and
remain unchanged with the size and shape of the surface.
Alternatively- The total number of electric field lines emanating from
the enclosed charge „qβ€Ÿ are same for all surfaces 1,2 &3
½
½
(b)
𝜎
2𝜎
π‘œ
πœ–π‘œ
We have 𝐸1 = πœ– ; 𝐸2 =
(i) Between the plates
𝐸𝑖𝑛 = 𝐸1 + 𝐸2
Ajmer SET I Page 13 of 15
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Final Draft
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=
𝜎
2πœ– π‘œ
2𝜎
3𝜎
π‘œ
2πœ– π‘œ
+ 2πœ– =
½
(Directed towards sheet „2β€Ÿ)
(ii) Outside near the sheet „1β€Ÿ
πΈπ‘œπ‘’π‘‘ = 𝐸2 − 𝐸1
2𝜎
𝜎
𝜎
= 2πœ– − 2πœ– = 2πœ–
.
π‘œ
π‘œ
½
5
π‘œ
(Directed towards sheet „2β€Ÿ)
OR
a) Definition of electrostatic potential and SI unit
1+½
Derivation for the electrostatic potential energy
b) Equipotential surface for (i) & (ii)
1+½
1+1
a) Electrostatic potential : Work done by an external force in bringing a
unit positive charge from infinity to the given point
SI unit- volt or J/C)
Net work done in moving charges π‘ž1 . π‘ž2 &π‘ž3 from infinity to A, B and
C respectively
5
1
½
π‘Š = 0 + π‘ž2 𝑉13 + π‘ž3 (𝑉13 𝑉23 )
=
1
π‘ž1 π‘ž2
4πœ‹πœ– 0
π‘Ÿ12
+
1
4πœ‹πœ– 0
(
π‘ž1 π‘ž3
π‘Ÿ13
+
π‘ž2 π‘ž3
π‘Ÿ23
½
)
But potential energy of the system is equal to the work
done.
1
π‘ž1 π‘ž2 π‘ž1 π‘ž3 π‘ž2 π‘ž3
∴π‘ˆ=𝑀=
(
+
+
)
4πœ‹πœ–0 π‘Ÿ12
π‘Ÿ13
π‘Ÿ23
(Award these 1 mark if the student directly writes the expression
for π‘ˆ)
½
½
(b) Equipotential surface due to
(i)
An electric dipole
1
Ajmer SET I Page 14 of 15
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(ii)
Two identical positive changes
1
5
2
Ajmer SET I Page 15 of 15
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