SOLVED: Problem-2 (60 points): The deflection y in a simply supported beam with uniform load and tensile axial load T is given bydy/dx = (Ty)/(q(L-x)) * (1/(E*I)) * (1/2) * (x^2 - L*x^2)where x is the location along the beam (in), T is the tension applied (lbs), E is the Young modulus of elasticity of the beam (psi), I is the second moment of area (in^4), and q is the uniform loading intensity (lb/in). L is the length of the beam (in). The simply supported beam is shown in the following figure:G
SOLVED: Problem-2 (60 points): The deflection y in a simply supported beam with uniform load and tensile axial load T is given bydy/dx = (Ty)/(q(L-x)) * (1/(E*I)) * (1/2) * (x^2 -
VIDEO ANSWER: The calculation of the principal stress is the first thing that we need to appreciate when answering this question. The square root of the x dire…
numerade.com2022年5月11日
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SOLVED: Figure below shows a cantilever beam subjected to an axial compressive load of 450 kN acting at the center of the cross section, and two concentrated loads of 1.5P and P respectively, as shown in the Figure. The beam section is a solid rectangular section 150 mm wide and 300 mm deep. 1.1 Calculate the magnitude of the load (P) if the maximum tensile bending stress is 0.15 MPa. 1.2 Calculate the stresses due to bending, due to axial loading, and the resultant stresses. 1.3 Sketch the stre
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