A S Determine the maximum tensile stress at point A Gastension.A (MPa) due to external loads...

  

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A S Determine the maximum tensile stress at point A Gastension.A (MPa) due to external loads given in the figure. Notes: Point A is fixed and point D is roller supported. Also, there is a hinge at point B of the beam. Distributed load q (kN/m) is acting in-between point B and D in x-y plane, Point load P (kN) is acting from point C in z-x plane. The distance between point C and point D is also given as L. Cross section of the beam is given for section a-a. It is constant and valid for all parts of the structure. Also, elastic modulus is constant. Use your own values for solution. hinge B q (kN/m) P (KN) L a Omax,tension, A (MPa)= a Results Table X Z4- P (KN), +4 q (kN/m) b a-a Section A S Determine the maximum tensile stress at point A Gastension.A (MPa) due to external loads given in the figure. Notes: Point A is fixed and point D is roller supported. Also, there is a hinge at point B of the beam. Distributed load q (kN/m) is acting in-between point B and D in x-y plane, Point load P (kN) is acting from point C in z-x plane. The distance between point C and point D is also given as L. Cross section of the beam is given for section a-a. It is constant and valid for all parts of the structure. Also, elastic modulus is constant. Use your own values for solution. hinge B q (kN/m) P (KN) L a Omax,tension, A (MPa)= a Results Table X Z4- P (KN), +4 q (kN/m) b a-a Section