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Structural Beam Bending & Stress Inversion (Mechanical Engineering)

In solid mechanics and structural engineering, statically indeterminate structural beams subjected to asymmetric lateral and point loads develop internal bending moments M(x)M(x) that vary along the beam's longitudinal span. Under Euler-Bernoulli beam theory, the vertical deflection curve w(x)w(x) is related to the bending moment by M(x)=EIwβ€²β€²(x)M(x) = E I w''(x), where EE is Young's modulus and II is the area moment of inertia.

A mechanical engineer is analyzing an overhead gantry crane support girder of length L=6Β metersL = 6\text{ meters}. Under operating crane carriage loads, the internal bending moment distribution M(x)M(x) (in kNβ‹…m\text{kN}\cdot\text{m}) as a function of position x∈[0,6]x \in [0, 6] along the girder is modeled by the cubic polynomial:

M(x)=2x3βˆ’18x2+40xM(x) = 2x^3 - 18x^2 + 40x

  1. Find the roots of M(x)=0M(x) = 0 along the girder span [0,6][0, 6] to locate the neutral load pinning stations (xx-intercepts).
  2. Calculate the first derivative Mβ€²(x)M'(x) (representing internal shear force V(x)=dMdxV(x) = \frac{dM}{dx}), locate all stationary critical points, and classify local peak and valley bending moments using the First Derivative Test.
  3. Compute the second derivative Mβ€²β€²(x)M''(x), determine the intervals of concavity, and find the coordinates of all points of inflection.
  4. In structural design, a point of inflection in the deflection curve (wβ€²β€²(x)=0β€…β€ŠβŸΊβ€…β€ŠM(x)=0w''(x) = 0 \iff M(x) = 0) marks a point of contraflexure where internal stresses invert between upper-flange compression and upper-flange tension. Explain why identifying inflection points in M(x)M(x) governs the optimal placement of welded steel web stiffeners to prevent localized shear buckling.