The principal strains in a plane, measured experimentally at a point on the aluminum fuselage of a jet aircraft, are ε1 = 60 x 10-6, and ε2 = 210 x 10-6. If this is a case of plane stress, determine the associated principal stresses at the point in the same plane. E(al)= 10(10^3)ksi V(al)= 0.33
The principal strains in a plane, measured experimentally at a point on the aluminum fuselage of a jet aircraft, are ε1 = 60 x 10-6, and ε2 = 210 x 10-6. If this is a case of plane stress, determine the associated principal stresses at the point in the same plane. E(al)= 10(10^3)ksi V(al)= 0.33
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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The principal strains in a plane, measured experimentally at a point on the aluminum fuselage of a jet aircraft, are ε1 = 60 x 10-6, and ε2 = 210 x 10-6. If this is a case of plane stress, determine the associated principal stresses at the point in the same plane.
E(al)= 10(10^3)ksi
V(al)= 0.33
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