Hello All,
I'm new here, literally just joined! I am currently working on my "ticket to fly" as well working on a design modification for an experimental build. My question is this, what would be the best tail configuration for a bush plane? As a Florida native who has built and owned virtually every machine possible to "run the 'glades" aka, airboats, full-tracks, half-tracks, buggies, 4x4's etc etc I am always concerned with ground clearance. What I predominantly see on bush planes is a conventional tail meaning vertical rudder and low mounted -inline with fuselage- horizontal stabilizer. I understand the Piper Cub has a great deal of design influence, simply put it works and continues to work. That said, wouldn't a t-tail or v-tail be better in preventing damage to the leading edge of a low hanging wing? In my mind raising anything low hanging is a bonus. Just curious if aerodynamic concerns are dictating BCP tail design or is complacent acceptance of the design the norm? I view a strutless high wing with either a t or v tail to be far more resilient and resistant to damage than current designs or....am I merely over thinking this? Thanks!


