Various Rounded corner equilateral triangular shapes for different í µí¼ ¶ Shape functions for parabolically curved orthotropic triangular section (Fig.45) í µí± 1 = í µí¼‰(2í µí¼‰ − 1); í µí± 2 = í µí¼‚(2í µí¼‚ − 1); í µí± 3 = (1 − í µí¼‰ − í µí¼‚)(1 − 2í µí¼‰ − 2 í µí¼‚) (144) í µí± 4 = 4í µí¼‰í µí¼‚; í µí± 5 = 4í µí¼‚(1 − í µí¼‰ − í µí¼‚); í µí± 6 = 4í µí¼‰(1 − í µí¼‰ − í µí¼‚) For any ′í µí»¼′ the coordinates of the equilateral triangular plate with curved corners and the radius of the inner circle a=1 is shown in Fig.44 and the coordinates of the six nodes are given for í µí»¼ = 0.4 as í µí±¥ í µí± = [1 , −0.5, −0.5, 1 1+√í µí»¼ , − 2 1+√í µí»¼ , 1 1+√í µí»¼ ] = [1 − 0.5 − 0.5 0.6125 − 1.225 0.6125] (145a) í µí±¦ í µí± = [0 , 0.866 , −0.866, √3 1+√í µí»¼ , 0 , −√3 1+√í µí»¼ ] = [0 0.866 − 0.866 1.061 0 − 1.061]

Various Rounded corner equilateral triangular shapes for different í µí¼ ¶ Shape functions for parabolically curved orthotropic triangular section (Fig.45) í µí± 1 = í µí¼‰(2í µí¼‰ − 1); í µí± 2 = í µí¼‚(2í µí¼‚ − 1); í µí± 3 = (1 − í µí¼‰ − í µí¼‚)(1 − 2í µí¼‰ − 2 í µí¼‚) (144) í µí± 4 = 4í µí¼‰í µí¼‚; í µí± 5 = 4í µí¼‚(1 − í µí¼‰ − í µí¼‚); í µí± 6 = 4í µí¼‰(1 − í µí¼‰ − í µí¼‚) For any ′í µí»¼′ the coordinates of the equilateral triangular plate with curved corners and the radius of the inner circle a=1 is shown in Fig.44 and the coordinates of the six nodes are given for í µí»¼ = 0.4 as í µí±¥ í µí± = [1 , −0.5, −0.5, 1 1+√í µí»¼ , − 2 1+√í µí»¼ , 1 1+√í µí»¼ ] = [1 − 0.5 − 0.5 0.6125 − 1.225 0.6125] (145a) í µí±¦ í µí± = [0 , 0.866 , −0.866, √3 1+√í µí»¼ , 0 , −√3 1+√í µí»¼ ] = [0 0.866 − 0.866 1.061 0 − 1.061]

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This study focuses on the determination of torsional rigidity and maximum shear stresses in arbitrarily shaped isotropic and orthotropic composite sections with functional grading of material. A series of numerical examples are solved to validate this approach, with a comprehensive parametric study also conducted. The paper presents the practical a...

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