My question is generated from the idea of setting up my plane to fit mmy style of flying. I have replaced the tires with 8-6s. this really made the grass landings and rough taxing so much smoother. as a result of the increased AOA i was able to really shorten the take off roll and lift off at a lower speed. i then level out in ground effect to gain safe margin. I then replaced the tail wheel with a scott inflatable model. This has to be one of the best things that i have done to the plane. The tail now more easily rolls over clumpy grass and uneven pavement so much better. the plane picks up speed in rough grass better and i have eliminated the horrendous sound due to the hard wheel. unfortunately this tail wheel has raised my tail enough to increase my takeoff roll considerably and speed for lift off. I am debating new tire sizes as i would like to go to 29 or 26.
the question is: is there an optimum AOA for shortest takeoff? I am under the assumption that if the AOA is greater than or equal to stall speed you will achieve the lowest takeoff speed thus shortening the required distance.
would it be reasonable to take an angle measurement static and another at or very near power on stall speed. then using the new angle to set as the static angle either made up with tire height or extended legs?
the question is: is there an optimum AOA for shortest takeoff? I am under the assumption that if the AOA is greater than or equal to stall speed you will achieve the lowest takeoff speed thus shortening the required distance.
would it be reasonable to take an angle measurement static and another at or very near power on stall speed. then using the new angle to set as the static angle either made up with tire height or extended legs?
Comment