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
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
Problem 6.2P
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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.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F4e8acadd-1a1a-46cf-a6b9-1de43837e9f2%2Fa5dd9db3-e9db-415d-be81-3a45268f0d34%2F4bo3mz9_processed.jpeg&w=3840&q=75)
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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