Q-1 The principal strains in a plane, measured experimentally at a point on the aluminum fuselage of a jet aircraft, are ɛ1 = (your roll number +100) x 106 , and ɛ2 = (your roll number + 150) x 106. If this is a case of plane stress, determine the associated principal stresses at the point in the same plane. %3D 0.33. Eal 10(10³) ksi Val %3D

Structural Analysis
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Chapter2: Loads On Structures
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put 58 in roll no. thanks.

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Q-1 The principal strains in a plane, measured experimentally at a point on the aluminum
fuselage of a jet aircraft, are ɛ = (your roll number +100) x 106 , and ɛ2 = (your roll number +
150) x 106. If this is a case of plane stress, determine the associated principal stresses at the
point in the same plane.
E = 10(103) ksi
Val
0.33.
Transcribed Image Text:ur Q-1 The principal strains in a plane, measured experimentally at a point on the aluminum fuselage of a jet aircraft, are ɛ = (your roll number +100) x 106 , and ɛ2 = (your roll number + 150) x 106. If this is a case of plane stress, determine the associated principal stresses at the point in the same plane. E = 10(103) ksi Val 0.33.
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