Q-1 The principal strains in a plane, measured experimentally at a point on the aluminum fuselage of a jet aircraft, are ɛ = (41 +100) x 10- and ɛ2 = (41 + 150) x 106. If this is a case of plane stress, determine the associated principal stresses at the point in the same plane. Ea = 10(10) ksi Val = 0.33. %3D %3D

Materials Science And Engineering Properties
1st Edition
ISBN:9781111988609
Author:Charles Gilmore
Publisher:Charles Gilmore
Chapter6: Introduction To Mechanical Properties
Section: Chapter Questions
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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 = (41 +100) x 10-_, and ɛ2 = (41+ 150) x 10-6. If this is a case
of plane stress, determine the associated principal stresses at the point in the same plane.
Eal =
10(10) ksi val = 0.33.
Transcribed Image Text:Q-1 The principal strains in a plane, measured experimentally at a point on the aluminum fuselage of a jet aircraft, are ɛ = (41 +100) x 10-_, and ɛ2 = (41+ 150) x 10-6. If this is a case of plane stress, determine the associated principal stresses at the point in the same plane. Eal = 10(10) ksi val = 0.33.
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