If SM = 0.12 and cg is located at 20% chord from l.e. then, find appropriate neutral point location.
(a) 0.32
(b) 0.87
(c) 2.3
(d) 1.54
This question was addressed to me by my school teacher while I was bunking the class.
Origin of the question is Longitudinal Static Stability and Control-2 topic in chapter Stability, Control, and Handling Qualities of Aircraft Design