[ q = \fracT2A_m \quad \text(constant around section) ]
[ \sigma_bending = \fracM_y zI_xx + \fracM_z yI_yy ] aircraft structures lecture notes pdf
[ q = \fracV \cdot QI ]
This is the "meat" of most aircraft structures courses. Aircraft are essentially hollow tubes with wings to save weight. Lecture notes will focus heavily on: [ q = \fracT2A_m \quad \text(constant around section)