Stresses on the Principal Planes 6 the Planes of maximum shearing stress the Planes whose normals are at (+36.8°) and (+126.8°) with x-axis? show the results of Parts a, b and C on complete sketches of differential elements. юompa Ans/ @max = 40 MPa, min=-18 MPa, 0 = +21₁8° 32мра в Tmax=29MPa, Tmin=-29 May @= +66.8° 6x² = 11 MPa, 6y` = 11m Pa © 6 = 36₁1 MPa, I = 14.5 MPa 6² = -14.1 MPa, C²` = -14.5 MPa yo 20MP lompa 20MPa * 32 мра

Structural Analysis
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Chapter2: Loads On Structures
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A State of stress is specified as shown, Determine the normal and shearing.
Stresses on the Principal Planes 6 the Planes of maximum shearing stress the
Planes whose normals are at (+36.8°) and (+126.8°) with x-axis? show the
results of Parts a, b and C on complete sketches of differential elements.
TOM Pa
Ans/@max=40MPa, min=-18 MPa, 0 = +21.8°
b) Tmax=29MPa, Tmin=-29 MPa 0 = +66.8°
32 M 4
6x² = 11 MPa, 6y` = || MPa
© 6 = 36₁1 MPa, I = 14.5 MPa
6² = -14.1 MPa, C²` = -14.5 MPa
+2
yo
20MP
lompa
20Ma
32 MP
Transcribed Image Text:A State of stress is specified as shown, Determine the normal and shearing. Stresses on the Principal Planes 6 the Planes of maximum shearing stress the Planes whose normals are at (+36.8°) and (+126.8°) with x-axis? show the results of Parts a, b and C on complete sketches of differential elements. TOM Pa Ans/@max=40MPa, min=-18 MPa, 0 = +21.8° b) Tmax=29MPa, Tmin=-29 MPa 0 = +66.8° 32 M 4 6x² = 11 MPa, 6y` = || MPa © 6 = 36₁1 MPa, I = 14.5 MPa 6² = -14.1 MPa, C²` = -14.5 MPa +2 yo 20MP lompa 20Ma 32 MP
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