Calculate shell section like wing type of aircraft.
1. To determine normal and shear stresses. Draw plots ?z? q.
2. To determine the coordinates of the center of bending.
3. To determine the running angle of torsional deflection.
1. To determine normal and shear stresses. Draw plots ?z? q.
2. To determine the coordinates of the center of bending.
3. To determine the running angle of torsional deflection.
Can't find what you're looking for?