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Mechanical Properties of Solids Practice Questions - DPP for NEET

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1. (a). Y = 
2
MgL
r pDl
but Mg/pr
2
 = 20 × 10
8
  & Dl = L then
 Y = 20 × 10
8
 N/m
2
2. (b). F = Y a DtA
A = 2 × 10
–6
 m
2
, Y = 2 × 11 N/m
2
a = 1.1 × 10
–5
, t = 50 – 30 = 20°C
F = 2 × 10
11
 × 1.1 × 10
–5
 × 20 × 2 × 10
–6
 = 88N.
3. (d). Work done on the wire
W =
1
2
 F × l = 
1
2
 × stress x volume x strain
W =
1
2
 × Y × strain
2
 × volume
W = 
1
2
 × Y × 
2
2
L
D l
 × AL = 
2
YAL
2L
D
W = 
11 66
2 10 10 10
21
--
´ ´´
´
 = 0.1 J
4. (d). W = 
1
2
 ×  load × elongation
W = 
1
2
 × 5.4 × 10
6
 × 3
W = 8.1 × 10
6
 ergs
5. (d). By Hook's law
Y = 
F / A FL
/LA
=
ll
Y = 
82
161
(4 10 ) (0.2 10 )
--
´
´´
 = 2 × 10
11
 N/m
2
6. (a).  B = – 
PV
V
D
D
Given, DP = hdg = 200 x 10
3
 x 10
DP = 2 × 10
5
 N/m
2
V 0.1
V 100
D
= = 10
–3
\ B = 
6
3
2 10
10
-
´
 = 2 × 10
9
 N/m
2
7. (b). Y = 
stress F/ A FL
strain / L A
==
ll
\ l = 
3 2 11
FL 209.84
AY
(10 ) 1.96 10
-
´´
=
p´ ´´
  = 1.27 × 10
–3
 m = 1.27 mm
8. (a). Limiting stress = 4.0 × 10
8
 N/m
2
F 400
AA
= = 4.0 × 10
8
or   A = 10
–6
 m
2
\  D = 
1/2
1/2 6
4 A 4 10
-
æö
´ æö
=
ç÷ ç÷
èø
pp
èø
       = 1.13 × 10
–3
 m = 1.13 mm
9. (c). Stress = 
3
42
F 4.8 10N
A
1.2 10 m
-
´
=
´
 = 4.0 × 10
7
 N/m
2
10. (c). Strain = 
3
1 10
2
-
D´
=
l
l
 = 5 × 10
–4
, longitudinal
11. (c). F = Y A a Dt
       = 2 × 10
11
 × 3 × 10
–6
 × 10
-5
 × 20
    F = 120 N.
12. (c).   Compressibility
c = 
1V
K Vp
D
=-
D
 = 5 × 10
–10
\ Fractional decrease in volume
= –
V
V
D
= c D p = 5 × 10
–10
 × 15 × 10
6
           = 7.5 × 10
–3
13. (c). Increase in length on heating Dl = a L DT
To annul this increase if pressure applied is p then
  p = Y 
L
D l
= Ya DT
= 2 × 10
11
 × 1.1 × 10
–5
 × 100 = 2.2 × 10
8
 N/m
2
14. (c).  y = 2h (1 + s)
y = 2.4 × h
2.4 h = 2h (1 + s)
(1 + s) = 1.2
s = 0.2
15. (c).  Stress = F/A = 10/(2 × 10
-6
)  = 5 × 10
6
 N/m
2
Strain = 
6
11
Stress 5 10
Y
2 10
´
=
´
 = 2.5 × 10
–5
l = L × strain = 1 × 2.5 × 10
–5
l = 2.5 × 10
–5
 m
16. (b).   
12
Mg 1000 980 100
L AY
10 0.01
D ´´
==
´
l
Dl = 0.0098 cm.
17. (a). V olume = Mass/density
Area of cross-section = volume/length
Page 2


1. (a). Y = 
2
MgL
r pDl
but Mg/pr
2
 = 20 × 10
8
  & Dl = L then
 Y = 20 × 10
8
 N/m
2
2. (b). F = Y a DtA
A = 2 × 10
–6
 m
2
, Y = 2 × 11 N/m
2
a = 1.1 × 10
–5
, t = 50 – 30 = 20°C
F = 2 × 10
11
 × 1.1 × 10
–5
 × 20 × 2 × 10
–6
 = 88N.
3. (d). Work done on the wire
W =
1
2
 F × l = 
1
2
 × stress x volume x strain
W =
1
2
 × Y × strain
2
 × volume
W = 
1
2
 × Y × 
2
2
L
D l
 × AL = 
2
YAL
2L
D
W = 
11 66
2 10 10 10
21
--
´ ´´
´
 = 0.1 J
4. (d). W = 
1
2
 ×  load × elongation
W = 
1
2
 × 5.4 × 10
6
 × 3
W = 8.1 × 10
6
 ergs
5. (d). By Hook's law
Y = 
F / A FL
/LA
=
ll
Y = 
82
161
(4 10 ) (0.2 10 )
--
´
´´
 = 2 × 10
11
 N/m
2
6. (a).  B = – 
PV
V
D
D
Given, DP = hdg = 200 x 10
3
 x 10
DP = 2 × 10
5
 N/m
2
V 0.1
V 100
D
= = 10
–3
\ B = 
6
3
2 10
10
-
´
 = 2 × 10
9
 N/m
2
7. (b). Y = 
stress F/ A FL
strain / L A
==
ll
\ l = 
3 2 11
FL 209.84
AY
(10 ) 1.96 10
-
´´
=
p´ ´´
  = 1.27 × 10
–3
 m = 1.27 mm
8. (a). Limiting stress = 4.0 × 10
8
 N/m
2
F 400
AA
= = 4.0 × 10
8
or   A = 10
–6
 m
2
\  D = 
1/2
1/2 6
4 A 4 10
-
æö
´ æö
=
ç÷ ç÷
èø
pp
èø
       = 1.13 × 10
–3
 m = 1.13 mm
9. (c). Stress = 
3
42
F 4.8 10N
A
1.2 10 m
-
´
=
´
 = 4.0 × 10
7
 N/m
2
10. (c). Strain = 
3
1 10
2
-
D´
=
l
l
 = 5 × 10
–4
, longitudinal
11. (c). F = Y A a Dt
       = 2 × 10
11
 × 3 × 10
–6
 × 10
-5
 × 20
    F = 120 N.
12. (c).   Compressibility
c = 
1V
K Vp
D
=-
D
 = 5 × 10
–10
\ Fractional decrease in volume
= –
V
V
D
= c D p = 5 × 10
–10
 × 15 × 10
6
           = 7.5 × 10
–3
13. (c). Increase in length on heating Dl = a L DT
To annul this increase if pressure applied is p then
  p = Y 
L
D l
= Ya DT
= 2 × 10
11
 × 1.1 × 10
–5
 × 100 = 2.2 × 10
8
 N/m
2
14. (c).  y = 2h (1 + s)
y = 2.4 × h
2.4 h = 2h (1 + s)
(1 + s) = 1.2
s = 0.2
15. (c).  Stress = F/A = 10/(2 × 10
-6
)  = 5 × 10
6
 N/m
2
Strain = 
6
11
Stress 5 10
Y
2 10
´
=
´
 = 2.5 × 10
–5
l = L × strain = 1 × 2.5 × 10
–5
l = 2.5 × 10
–5
 m
16. (b).   
12
Mg 1000 980 100
L AY
10 0.01
D ´´
==
´
l
Dl = 0.0098 cm.
17. (a). V olume = Mass/density
Area of cross-section = volume/length
60
DPP/ P 20
=
mass
density length ´
 =
3
15.6 10
7800 2.5
-
´
´
 = 8 × 10
–7
 m
2
Y = 
73
F 8 9.8 2.5
AL
(8 10 ) 1.25 10
--
´´
=
D
´ ´´
l
Y = 1.96 × 10
11
 N/m
2
18. (c). Potential energy per unit volume = u
                 = 
1
2
× stress × strain
But    Y = 
stress
strain
\ stress = Y x strain = Y x S
\  Potential energy per unit volume = u
 = 
1
2
 × (YS)S = 
1
2
 YS
2
19. (d). 
2
1 12
2
2
21
Lr
Lr
=
l
l
L
1
 = L, L
2
 = 2L, r
1
 = 2R., r
2
 = R
\  
2
1
2
2
LR1
.
2L8
4R
==
l
l
20. (c). stress = 
2
ForceF
Area
r
=
p
\ stress S µ
2
1
r
\ 
2
12
21
Sr
Sr
æ ö æö
=
ç ÷ ç÷
è ø èø
Given 
1
2
r 2
r1
=
  \
1
2
S 1
S4
=
21. (c) F YA FA = aDq\µ
22. (a) For twisting, angle of shear 
1
L
fµ
i.e. if L is more then f will be small.
23. (a) ( ) Y 21 = h +s
24. (a) 
( )
0.5Y
Y 21
-h
= h +s Þ s=
h
25. (a) Tensile stress 
2
Fcos Fcos
a/cosa
qq
==
q
26. (a) Tensile stress is maximum when 
2
cos q
 is maximum,
i.e., 
0 q=°
27. (b) Shearing stress
Fsin Fsin cos
a/cosa
q qq
==
q
Fsin2
2a
q
=
28. (a) Elasticity is a measure of tendency of the body to regain
its original configuration. As steel is deformed less than
rubber therefore steel is more elastic than rubber.
29. (a) Bulk modulus of elasticity measures how good the body
is to regain its original volume on being compressed.
Therefore, it represents incompressibility of the material.
PV
K
V
-
=
D
 where P is increase in pressure, DV is change
in volume.
30. (a) A bridge during its use undergoes alternating strains
for a large number of times each day , depending upon the
movement of vehicles on it when a bridge is used for long
time, it losses its elastic strength. Due to which the amount
of strain in the bridge for a given stress will become large
and ultimately, the bridge may collapse. This may not
happen, if the bridges are declared unsafe after long use.
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FAQs on Mechanical Properties of Solids Practice Questions - DPP for NEET

1. What are the different types of mechanical properties of solids?
Ans. The different types of mechanical properties of solids include elasticity, plasticity, ductility, brittleness, hardness, toughness, and strength. These properties determine how a solid responds to external forces and deformation.
2. How is elasticity defined in the context of mechanical properties of solids?
Ans. Elasticity is the ability of a material to regain its original shape and size after the removal of external forces that caused deformation. It is characterized by the material's ability to store and release energy elastically, without undergoing permanent deformation.
3. What is the difference between ductility and brittleness?
Ans. Ductility refers to the ability of a material to undergo plastic deformation before fracture. Ductile materials can be drawn into wires or stretched without breaking easily. On the other hand, brittleness refers to the tendency of a material to fracture or break without undergoing significant plastic deformation. Brittle materials are prone to sudden failure and do not exhibit much plasticity.
4. How is hardness measured in the context of mechanical properties of solids?
Ans. Hardness is a measure of a material's resistance to indentation or scratching. It is usually determined using tests such as the Mohs scale or the Vickers hardness test. The hardness of a material is influenced by its atomic structure, crystal lattice, and the strength of its interatomic bonds.
5. What is the relationship between strength and toughness in mechanical properties of solids?
Ans. Strength and toughness are both measures of a material's ability to resist external forces and deformation. However, strength refers to the material's ability to withstand applied stress without failure, while toughness refers to its ability to absorb energy and deform plastically before fracture. A material can be strong but not tough, or tough but not strong, depending on its composition and structure.
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