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The state of plane stress at a point in a loaded member is given by:
sx = + 800 MPa
sy = + 200 MPa
txy = ± 400 MPa
The maximum principal stress and maximum shear stress are given by:
  • a)
    smax = 800 MPa and tmax = 400 MPa
  • b)
    smax = 800 MPa and tmax = 500 MPa
  • c)
    smax = 1000 MPa and tmax = 500 MPa
  • d)
    smax = 1000 MPa and tmax = 400 MPa
Correct answer is option 'C'. Can you explain this answer?
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The state of plane stress at a point in a loaded member is given by:sx...
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The state of plane stress at a point in a loaded member is given by:sx...
The given problem states that the state of plane stress at a point in a loaded member is given by:

σx = 800 MPa
σy = 200 MPa
τxy = 400 MPa

To find the maximum principal stress (σmax) and maximum shear stress (τmax), we can use the following equations:

σmax = (σx + σy)/2 + √(((σx - σy)/2)^2 + τxy^2)
τmax = √(((σx - σy)/2)^2 + τxy^2)

Let's calculate the values:

σmax = (800 + 200)/2 + √(((800 - 200)/2)^2 + 400^2)
= 1000 MPa

τmax = √(((800 - 200)/2)^2 + 400^2)
= √((300)^2 + 400^2)
= √(90000 + 160000)
= √250000
= 500 MPa

Therefore, the maximum principal stress (σmax) is 1000 MPa and the maximum shear stress (τmax) is 500 MPa.

Hence, the correct answer is option (c): σmax = 1000 MPa and τmax = 500 MPa.
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The state of plane stress at a point in a loaded member is given by:sx = + 800 MPasy = + 200 MPatxy = ± 400 MPaThe maximum principal stress and maximum shear stress are given by:a)smax = 800 MPa and tmax = 400 MPab)smax = 800 MPa and tmax = 500 MPac)smax = 1000 MPa and tmax = 500 MPad)smax = 1000 MPa and tmax = 400 MPaCorrect answer is option 'C'. Can you explain this answer?
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