For the configuration shown in Fig. P6.11, determine the deflection at the point of load application...

 

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For the configuration shown in Fig. P6.11, determine the deflection at the point of load application using a one-element model. If a mesh of several triangular elements is used, comment on the stress values in the elements close to the tip. 90 N 35 mm 2 (0, 25) 45 N 1 (35, 25) 25 mm t = 8 mm E = 69 900 MPa v = 0.3 FIGURE P6.11 For the configuration shown in Fig. P6.11, determine the deflection at the point of load application using a one-element model. If a mesh of several triangular elements is used, comment on the stress values in the elements close to the tip. 90 N 35 mm 2 (0, 25) 45 N 1 (35, 25) 25 mm t = 8 mm E = 69 900 MPa v = 0.3 FIGURE P6.11