mkmuch
Active Member
Series of Questions...
The Set up - I am contemplating the rudder trim modification for the -10 now that I am nearing the end of my vert stab assembly. I have some questions about the various mods I see on several builder sites, thought I's just ask the team (that's you guys).
#1. What portion of the vert stab offers the most effectiveness to the aircraft? The bottom where it's longer, middle way up and medium length, or at the top where it's the smallest? Guess I am driving towards - is it the surface area of the vert, the position in the airstream, both or non of the above that offers the most efficiency?
#2. based on the answer to Q1 - is the answer the same for the rudder?
#3. Based on the answer to Q2 - Where is the optimal place to put an electric rudder trim section?
#4. For those that have done it (I have seen 2 methods - piano hinge hanging off the rudder about middle way up - and section the actual rudder control surface and incorporate the trim device into the rudder again about mid way up) is it just coincidence that you placed the rudder trim control surface mid way up or is there a method to it - see questions #1 & #2?
#5. Based on the variations of rudder trim solutions is there a formula for control surface area you want to achieve - i.e. the piano hinge clearly has less surface area than the sectioned in control surface?
#6. How about moment change for the rudder control surface? the servo and trim tab in the rudder have added extra weight to that control surface above what the counter weight was anticipating - does that manifest itself negatively in flight? Do you anticipate early hinge failure? Have you modified / beefed up the hinges to accommodate this change?
#7. How much drag do you anticipate this device with the control arm out in the airstream having on the overall performance of the aircraft - a couple of knots of speed?
#8. Has anyone spent anytime trying to engineer a piper Archer, Arrow, Cherokee type manual rudder trim knob into the plane? I am not intimate with the control type in the Piper so may not be compatible? The thought would be to turn the entire rudder into a self-trimming surface by manually or electrically moving the main rudder cables or pedals as is the case with the piper - thus eliminating the need for a trim tab all together?
#9. Am I over thinking the impacts of this - wait - Don't answer that one - already figured it out!
Sorry for the long post - just pondering and had to write it all down.
The Set up - I am contemplating the rudder trim modification for the -10 now that I am nearing the end of my vert stab assembly. I have some questions about the various mods I see on several builder sites, thought I's just ask the team (that's you guys).
#1. What portion of the vert stab offers the most effectiveness to the aircraft? The bottom where it's longer, middle way up and medium length, or at the top where it's the smallest? Guess I am driving towards - is it the surface area of the vert, the position in the airstream, both or non of the above that offers the most efficiency?
#2. based on the answer to Q1 - is the answer the same for the rudder?
#3. Based on the answer to Q2 - Where is the optimal place to put an electric rudder trim section?
#4. For those that have done it (I have seen 2 methods - piano hinge hanging off the rudder about middle way up - and section the actual rudder control surface and incorporate the trim device into the rudder again about mid way up) is it just coincidence that you placed the rudder trim control surface mid way up or is there a method to it - see questions #1 & #2?
#5. Based on the variations of rudder trim solutions is there a formula for control surface area you want to achieve - i.e. the piano hinge clearly has less surface area than the sectioned in control surface?
#6. How about moment change for the rudder control surface? the servo and trim tab in the rudder have added extra weight to that control surface above what the counter weight was anticipating - does that manifest itself negatively in flight? Do you anticipate early hinge failure? Have you modified / beefed up the hinges to accommodate this change?
#7. How much drag do you anticipate this device with the control arm out in the airstream having on the overall performance of the aircraft - a couple of knots of speed?
#8. Has anyone spent anytime trying to engineer a piper Archer, Arrow, Cherokee type manual rudder trim knob into the plane? I am not intimate with the control type in the Piper so may not be compatible? The thought would be to turn the entire rudder into a self-trimming surface by manually or electrically moving the main rudder cables or pedals as is the case with the piper - thus eliminating the need for a trim tab all together?
#9. Am I over thinking the impacts of this - wait - Don't answer that one - already figured it out!
Sorry for the long post - just pondering and had to write it all down.