doc: update comments
@@ -78,7 +78,8 @@ class LiftDistribution(BaseSolver):
lift_distribution = np.zeros((N_nodes, numb_col))
for inode in range(N_nodes):
if self.data.aero.aero_dict['aero_node'][inode]:
- lift_distribution[inode,3]=np.dot(rot.T, forces[inode, :3])[2] # lift force (z direction in A frame or B frame)
+ # transform forces from B to A frame
+ lift_distribution[inode,3]=np.dot(rot.T, forces[inode, :3])[2] # lift force
lift_distribution[inode,2]=struct_tstep.pos[inode, 2] #z
lift_distribution[inode,1]=struct_tstep.pos[inode, 1] #y
lift_distribution[inode,0]=struct_tstep.pos[inode, 0] #x
