You don't need to draw it in solidworks just use your hand nothing else.

Calculate shell section like wing type of aircraft. 1. To determine normal and shear stresses. Draw plots oz q. 2. To determine the coordinates of the center of bending. 3. To determine the running angle of torsional deflection. Input: 1=1,5,F=1,3F1=1,2F2,H1=0,5H Materials shall section: duralumin (E=7,2105kgcm2) Note: skin perceives normal stresses, 1 does not perceive normal stresses. Calculate shell section like wing type of aircraft. 1. To determine normal and shear stresses. Draw plots oz q. 2. To determine the coordinates of the center of bending. 3. To determine the running angle of torsional deflection. Input: 1=1,5,F=1,3F1=1,2F2,H1=0,5H Materials shall section: duralumin (E=7,2105kgcm2) Note: skin perceives normal stresses, 1 does not perceive normal stresses