A typical jet transport aircraft needs to be sized based on following parameters. Wing area S=50m^2, MAC=5m. If tail volume coefficient of horizontal tail is 1 and tail area is 10m^2 then, find the required tail moment arm.
(a) 25m
(b) 50m
(c) 25cm
(d) 65in
I had been asked this question in an interview.
This intriguing question originated from Geometry Sizing in section Initial Sizing of Aircraft Design