Mechanical Engineering - Strength of Materials - Discussion
Discussion Forum : Strength of Materials - Section 1 (Q.No. 7)
7.
A body is subjected to a tensile stress of 1200 MPa on one plane and another tensile stress of 600 MPa on a plane at right angles to the former. It is also subjected to a shear stress of 400 MPa on the same planes. The maximum normal stress will be
Discussion:
57 comments Page 3 of 6.
Abhishek said:
9 years ago
Thank you all for the explanation.
Atosh said:
9 years ago
The maximum and minimum normal stresses (σ1 and σ2) are known as the principal stresses.
Manoj Nayak said:
9 years ago
Solution is very simple. Ans is 1400.
Explanation:
Normal stress =((x+y)÷2) + √ ((x - y)÷2) + (shear stress)^2 where x = 1200 & y= 600.
Explanation:
Normal stress =((x+y)÷2) + √ ((x - y)÷2) + (shear stress)^2 where x = 1200 & y= 600.
Alham said:
9 years ago
If shear stress is applied, maximum normal stress will always be greater than applied maximum stress(1200). So the answer is 1400. No calculation only observation.
Rahul said:
9 years ago
Normal stress = (sum of stress/2) = 900 answer.
Seenu said:
9 years ago
Thanks for all your explanation.
Avneesh said:
9 years ago
You can also use this formula,
Stress = [(x + y)/2] + 0.5 * (x - y)^2 + 4(shear stress)^2.
Stress = [(x + y)/2] + 0.5 * (x - y)^2 + 4(shear stress)^2.
Naeem said:
9 years ago
Simply use Mohr's circle to the equations.
Yajat Sharma said:
10 years ago
Maximum. normal stress = T.S - S.S.
= T.S1 + T.S2 - S.S.
= 1200 + 600 - 400 .
= 1400 answer.
= T.S1 + T.S2 - S.S.
= 1200 + 600 - 400 .
= 1400 answer.
Satyam jha said:
10 years ago
Principal stress are maximum and minimum normal stress which may be developed on a loaded bodyNormal Stress = (Shear Stress*sin2theta)+((Fx+Fy)/2)+(((Fx-Fy)/2)cos2theata).
In this Case theta = 90 because they are at right angle.
Other all values are given on calculation we get answer A)400.
Reference: Strength of materials by R.K.Rajput.
Chapter 2, Page NO.95 Eq.2.8..
Let, tensile stress on one plane(t.s1) = 1200mpa.
Tensile stress on another plane(t.s2) = 600mpa.
Shear stress (s.s) = 400mpa.
Now using major principal stress formula = [(t.s1+t.s2)/2]+sqrt[{(t.s1-t.s2)*(t.s1-t.s2)}/2 +(s.s*s.s)].
In this Case theta = 90 because they are at right angle.
Other all values are given on calculation we get answer A)400.
Reference: Strength of materials by R.K.Rajput.
Chapter 2, Page NO.95 Eq.2.8..
Let, tensile stress on one plane(t.s1) = 1200mpa.
Tensile stress on another plane(t.s2) = 600mpa.
Shear stress (s.s) = 400mpa.
Now using major principal stress formula = [(t.s1+t.s2)/2]+sqrt[{(t.s1-t.s2)*(t.s1-t.s2)}/2 +(s.s*s.s)].
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