Part A The stress at a point is shown on the element. Suppose that a = 105 MPa, T,, = 158 MPa . Determine the principal stress. (Figure 1) Enter your answers numerically using three significant figures separated by commas. A AEo vec Omax, Oint, Omin = MPa Submit Request Answer Part B Determine the absolute maximum shear stress. Express your answer with three significant figures and use the appropriate units. HA ? Figure < 1 of 1 Value Units Тmаx in-plane Submit Request Answer

Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
Section: Chapter Questions
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Part A
The stress at a point is shown on the element. Suppose that o, =
105 MPа, т - 158 MPа
Determine the principal stress.
(Figure 1)
Enter your answers numerically using three significant figures separated by commas.
VG AEo t vec
?
Omax, Oint, Omin =
MPа
Submit
Request Answer
Part B
Determine the absolute maximum shear stress.
Express your answer with three significant figures and use the appropriate units.
HA
O ) ?
Figure
1 of 1 >
Value
Units
Timax in-plane =
Submit
Request Answer
Provide Feedback
Transcribed Image Text:Part A The stress at a point is shown on the element. Suppose that o, = 105 MPа, т - 158 MPа Determine the principal stress. (Figure 1) Enter your answers numerically using three significant figures separated by commas. VG AEo t vec ? Omax, Oint, Omin = MPа Submit Request Answer Part B Determine the absolute maximum shear stress. Express your answer with three significant figures and use the appropriate units. HA O ) ? Figure 1 of 1 > Value Units Timax in-plane = Submit Request Answer Provide Feedback
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