- #1
jason.bourne
- 82
- 1
how is aspect ratio of a wing related to longitudinal static stability (LSS)?
like, if we increase the aspect ratio, is it going to increase or decrease the longitudinal static stability (LSS)?
suppose we have an aircraft whose centre of gravity is fixed at a particular location, if the propeller is mounted on the nose of the fuselage instead at the wing, what's its effect on LSS ?
like, if we increase the aspect ratio, is it going to increase or decrease the longitudinal static stability (LSS)?
suppose we have an aircraft whose centre of gravity is fixed at a particular location, if the propeller is mounted on the nose of the fuselage instead at the wing, what's its effect on LSS ?