Showing posts with label strain. Show all posts
Showing posts with label strain. Show all posts

Saturday, 4 February 2012

ADVANCED STRENGTH OF MATERIALS UNIT :4


UNIT :4 state of stress in 3 dimension
1) What are the types of failure?
The 2 types of failure are;
I. Brittle failure
II. Ductile failure
2) Define Brittle failure
Failure of a material represents direct separation of particles from each other, accompanied
by considerable deformation is known as Brittle failure.
3) Define ductile failure
Slipping of a material accompanied, by considerable plastic deformations is known as ductile
failure.
4) Define tensor
State of a stress at a point is defined by three components on each of the three mutually
perpendicular axis in mathematical terminology is called tensor.
5) List out the theories of failure
 Maximum principal stress theory(Rankine’s theory)
 Maximum principal strain theory(St.Venant’s theory)
 Maximum shear stress theory(Tresca’s & guest theory)
 Maximum shear strain energy theory(Von-Mises-Hencky theory)
 Maximum strain energy theory(Haigh’s theory)
6) Define Maximum principal stress theory (Rankine’s theory)
According to this theory, the failure of a material will occur when the maximum principal
tensile stress (σ1) in the complex system reaches the value of the maximum stress (σ t*) at the elastic
limit in simple tension or the minimum principal stress (i.e., the maximum principal compressive stress)
reaches the value of the maximum stress at the elastic limit in simple compression..
σ1= σ t*
7) Define Maximum principal strain theory (St.Venant’s theory)
According to this theory, the failure of a material will occur when the maximum principal strain
(e1) reaches the strain due to the yield stress in simple tension (σ t*/E).
e1= σ t*/E
In 3D e1= [σ1-μ (σ2+σ3)] = σ t*/E
In 2D e1= [σ1-μσ2] = σ t*/E
8) Define Maximum shear stress theory (Tresca’s & guest theory)
According to this theory, the failure of a material will occur when the maximum shear stress in
the body will reaches the value of Maximum shear stress in simple tension at the elastic limit.
In 3D (σ1- σ3) = σ t*
In 2D σ1 = σ t*
9) Define Maximum shear strain energy theory (Von-Mises-Hencky theory)
According to this theory, the failure of a material will occur when the total shear strain energy
per unit volume in the stressed material reaches a value equal to the shear strain energy per unit
volume at the elastic limit in simple tensile test.
In 3D shear strain energy due to distortion U = (1/12C) [(σ1- σ2) ^2+ (σ2- σ3) ^2+ (σ3- σ1) ^2]
In 3D shear strain energy due to simple tension U = σ t*^2\6C
U= (1/6C) [(σ1- σ2) ^2+ (σ2- σ3) ^2+ (σ3- σ1) ^2] = σ t*^2\6C
In 2D shear strain energy due to simple tension
U= (1/6C) [(σ1- σ2) ^2+ (σ2) ^2+ (σ1) ^2] = σ t*^2\6C
10) Define Maximum strain energy theory (Haigh’s theory)
According to this theory, the failure of a material will occur when the total strain energy per
unit volume in the stressed material reaches the strain energy per unit volume of the material at the
elastic limit in simple tensile test.
In 3D shear strain energy due to deformation
U= (1/2E) [σ1^2+ σ2^2+ σ3^2+-2μ (σ1σ2 +σ2σ3 +σ3 σ1)]
In 3D shear strain energy due to simple tension U= σ t*^2\2E
U= [σ1^2+ σ2^2+ σ3^2+-2μ (σ1σ2 +σ2σ3 +σ3 σ1)] = σ t*^2
In 2D U= [σ1^2+ σ2^2 -2μ (σ1σ2)] = σ t*^2
11) Write the limitations of Maximum principal stress theory (Rankine’s theory)
• This theory disregards the effect of other principal stresses & effect of shearing
stresses on other planes through the planes through the element.
• Material in tension test piece along 45º to the axis of the test piece, where normal
stress is neither maximum nor minimum, but the shear stress is maximum.
• Failure is not brittle but cleavage failure.
12) Write the limitations of shear stress theory (Tresca’s & guest theory)
This theory does not give accurate results for the state of stress of pure shear in which the
maximum amount of shear is developed (in torsion test).
13) Write the limitations of Maximum shear strain energy theory (Von-Mises-Hencky theory)
This theory cannot be applied to materials under hydro static pressure
14) Write the limitations Maximum strain energy theory (Haigh’s theory)
This theory does not apply to brittle materials for which elastic limit in tension and
compression is quite different.
15) Define strain Rosette
Linear strains are measured in all direction by strain gauges known as strain Rosette.
16) Define Plasticity ellipse
The graphical surface of a maximum shear strain energy theory (Von-Mises-Hencky theory) is
a straight circular cylinder.
[σ1^2+ σ2^2 -σ1σ2] = σ t*^2, which is called Plasticity ellipse.
17) Define Octahedral Plane
The plane which is equally inclined to the three axes of reference is called Octahedral Plane.
18) Define Octahedral Stresses
The normal and shear stress acting on the Octahedral Plane (The plane which is equally
inclined to the three axes of reference) is known as Octahedral Stresses.
19) Define volumetric strain per unit volume
Volumetric strain per unit volume is defined as the ratio of change in volume of a material to
its unit volume.
ev = ex +ey +ez
20) What are residual Stresses?
Maximum principal stress and Maximum shear stress are collectively known as residual
Stresses.

ADVANCED STRENGTH OF MATERIALS UNIT :1


1) Define Strain energy
When an elastic body is loaded with in an elastic limit, it deforms and some work is done which
is stored with in the body in the form of internal energy. This stored energy in the deformed body is
known as Strain energy.
2) Define Proof Resilience
Proof Resilience is the maximum energy stored in the body within the elastic limit.
3) Define Strain energy Density (Resilience)
The ability of the material to regain its original shape on removal of the applied load is known
as Strain energy Density (Resilience).
4) Define Modulus of Resilience
Proof Resilience per unit volume is known as Modulus of Resilience.
5) Write the formula to calculate the strain energy due to axial loads.
U=∫ P^2 dx limit 0 to L
2AE
Where,
P=Applied tensile load
L=length of the member
A=Area of the member
E=Young’s Modulus
6) Write the formula to calculate the strain energy due to bending
U=∫M^2 dx limit 0 to L
2EI
Where,
M=Bending moment due to applied loads
E=Young’s Modulus
I=moment of inertia
7) Write the formula to calculate the strain energy due to torsion in a solid shaft
U= V* (fs)^2
4N
Where,
Fs= maximum shear stress developed in the outermost layer.
V=volume of shaft
N= Modulus of rigidity
8) Write the formula to calculate the strain energy due to torsion in a Hollow shaft
U= fs^2(D^2+d^2)
4ND^2
Where,
Fs= maximum shear stress developed in the outermost layer.
D=outer diameter of the shaft
d=inner diameter of the shaft
N= Modulus of rigidity
9) Write the formula to calculate the strain energy if the moment value is given.
U=M^2
2EI
Where,
M=Bending moment due to applied loads
E=Young’s Modulus
I=moment of inertia
10) Write the formula to calculate the strain energy if the applied load value is given
U=P^2L
2AE
Where,
P=Applied tensile load
L=length of the member
A=Area of the member
E=Young’s Modulus
11) State Castigliano’s theorem
Castigliano’s theorem states that” If a body is acted upon by forces f1, f2, f3…..fn and U is the
strain energy stored in the body the partial derivative of the strain energy with respect to a force system
fi gives the displacement of the body in the direction of fi.
δi= ∂U
∂fi
12) What are the uses of Castigliano’s theorem?
i) To determine the deflection of complicated structures.
ii) To determine the deflection of curved beams and springs.
13) Define unit load method
The external loads are removed and the unit load is applied at places where deflection has to
be found out is known as unit load method.
14) Define Maxwell’s Reciprocal theorem
In any beam or truss the deflection at any point ‘A’ due to a load ‘W’ at any other point ‘C’ is
the same as the deflection at ’C’ due to the same load at ‘A’.
δA=δC
15) Compare the unit load method and Castigliano’s first theorem
In the unit load method one has to analyze the frame to find the load and deflection while
in the latter method, only one analysis is needed.
16) What is Williot Mohr’s diagram?
Williot Mohr’s diagram is a graphical method to find the deflection of the beam.
17) Write the formula for finding deflection of a fixed beam carrying a load w at the free end of length L
δ =wL^3
3EI
18) State the principal of virtual work
Direct use of deflection and strain energy for determining deflection of beam breaks down due
to several deflections. Hence an extraordinary device meant for solving this problem i.e., by replacing
true or real work and strain energy by external and internal work.
19) Write the formula for finding strain energy per unit volume due to a tensile stress (f)
U=f^2
2E
Where,
P= tensile stress
E=Young’s Modulus
20) Write the formula for finding deflection of a beam of length (L) simply supported at one end caries a
point load (W) at its centre.
δ = WL^3
48EI

Friday, 3 February 2012

machanics of solids important question


Part -B
1. A rectangular block of material is subjected to a tensile stress of 110 N/mm2 on one
plane and a tensile stress of 47 N/mm2 on the plane at right angle to the former.
Each of the above stress is accompanied by a shear stress of 63 N/mm2 Find (i)
The direction and magnitude of each of the principal stress (ii) Magnitude of
greatest shear stress.
2. At a point in a strained material, the principal stresses are100 N/mm2 (T) and 40
N/mm2 (C). Determine the resultant stress in magnitude and direction in a plane
inclined at 600 to the axis of major principal stress. What is the maximum intensity
of shear stress in the material at the point?
3. A cantilever truss is show in fig. Find the forces in the members of the truss by the
method of joint.
5 KN 10 KN
Error!
1.5m 3m
600
3m
4. A truss of span 9m is loaded as shown in fig. Find the reaction and forces in the
members marked 1, 2, and 3 by using method of section.
1
2 4m
3
3m 3m 3m
5. A thin cylindrical shell 3 m long has 1m internal diameter and 15 mm metal
thickness. Calculate the circumferential and longitudinal stresses induced and also
the change in the dimensions of the shell, if it is subjected to an internal pressure of
1.5 N/mm2 Take E = 2x105 N/mm2 and poison’s ratio =0.3. Also calculate change in
volume.
6. A closed cylindrical vessel made of steel plates 4 mm thick with plane ends, carries
fluid under pressure of 3 N/mm2 The diameter of the cylinder is 25cm and length is
75 cm. Calculate the longitudinal and hoop stresses in the cylinder wall and
determine the change in diameter, length and Volume of the cylinder. Take E =
2.1x105 N/mm2 and 1/m = 0.286.
7. Derive double integration method for cantilever beam concentrated load at free end.
8. A 2m long cantilever made of steel tube of section 150 mm external diameter and
10mm thick is loaded as show in fig If E=200 GN/m2 calculate (1) The value of W
so that the maximum bending stress is 150 MN/m2 (2) The maximum deflection for
the loading.
2W W
Error!
a = 0.5m
l = 2m
9. Determine the diameter of a solid shaft which will transmit 300 KN at 250 rpm. The
maximum shear stress should not exceed 30 N/mm2 and twist should not be more
than 10 in a shaft length 2m. Take modulus of rigidity = 1x 105N/mm2.
10. The stiffness of the closed coil helical spring at mean diameter 20 cm is made of 3
cm diameter rod and has 16 turns. A weight of 3 KN is dropped on this spring. Find
the height by which the weight should be dropped before striking the spring so that
the spring may be compressed by 18 cm. Take C= 8x104 N/mm2.
11. A compound tube consist of steel tube 140mm internal diameter and 160mm
external diameter and an outer brass tube 160mm internal diameter and 180mm
external diameter. The two tubes are of same length. The compound tube carries an
axial load of 900 KN. Find the stresses and the load carried by each tube and the
amount it shortens. Length of each tube is 140mm. Take E for steel as 2 x 105
N/mm2.
12. A rectangle block of material is subjected to a tensile stress of 110 N/mm2 on one
plane and a tensile stress of 47 N/mm2 on the plane at right angles to the former.
Each of the above stress is accompanied by shear stress of 63 N/mm2. Find (i) the
direction and magnitude of each of the principal stress (ii) magnitude of greatest
shear stress.
13. . At a point in a strained material, the principal stresses are 100 N/mm2 (T) and 40
N/mm2 (C) Determine the direction and magnitude in a plane inclined at 600 to the
axis of major principal stress. What is the maximum intensity of shear stress in the
material at the point
14. It is required to design a closed coiled helical spring which shall deflect 1mm under
an axial load of 100 N at a shear stress of 90 Mpa. The spring is to be made of
round wire having shear modulus of 0.8 x 105 Mpa. The mean diameter of the coil
is 10 times that of the coil wire. Find the diameter and length of the wire.
15. A steel shaft ABCD having a total length of 2400 mm is contributed by three
different sections as follows. The portion AB is hollow having outside and inside
diameters 80 mm and 50 mm respectively, BC is solid and 80 mm diameter. CD is
also solid and 70 mm diameter. If the angle of twist is same for each section,
determine the length of each portion and the total angle of twist. Maximum
permissible shear stress is 50 Mpa and shear modulus 0.82 x 105 MPa
16. Three planks of each 50 x200 mm timber are built up to a symmetrical I section for
a beam. The maximum shear force over the beam is 4KN. Propose an alternate
rectangular section of the same material so that the maximum shear stress
developed is same in both sections. Assume then width of the section to be 2/3 of
the depth.
17. Obtained the deflection under the greater load for the beam shown in fig using the
conjugate beam method.
60 KN 120 KN
2m 3m 1m
18. A beam of uniform section 10 m long carries a udl of KN/m for the entire length
and a concentrated load of 10 KN at right end. The beam is freely supported at the
left end. Find the position of the second support so that the maximum bending
moment in the beam is as minimum as possible. Also compute the maximum
bending moment,