Bill Harris
Jan 30, 2004, 04:08 PM
I have a Great Planes Yard Stick ARF slowflyer that I am prepping for use as an aerial photography platform.
Since I will be carrying more weight with the camera, larger battery and motor, and wing/airframe strengthening I plan to install a supplemental CF spar/wing joiner at the 33% chord point. This mod is still "on the board" and I've not finalized it, yet.
The weight will increase from 12 oz to 20 ounces, and the wing loading from 3.5 ounces/ft^2 to 5.8 ounces/ft^2.
One area of concern is the wing incidence.
The tailplane is at -0- degrees, the wing incidence at the root is 5.3 degrees, with the wing tip incidence at 3.5 degrees (washout twisted into the wing). The stock engine down-thrust is 6.6 degrees.
The airfoil is flatbottomed with a thickness of 5%. I think that the large wing incidence is present because it is a slow flyer and it might cause problems when the airspeed in increased with load. The wing incidence will be fixed once things are glued together and will not be easy to change. My intuition hints that the wing incidence ought to be reduced by a couple of degrees to 3.3 at the root to 1.5 at the wingtip.
Reports from others suggest that the engine downthrust should be reduced to -3 degrees.
What advice do we have on this situation?
--Bill
Since I will be carrying more weight with the camera, larger battery and motor, and wing/airframe strengthening I plan to install a supplemental CF spar/wing joiner at the 33% chord point. This mod is still "on the board" and I've not finalized it, yet.
The weight will increase from 12 oz to 20 ounces, and the wing loading from 3.5 ounces/ft^2 to 5.8 ounces/ft^2.
One area of concern is the wing incidence.
The tailplane is at -0- degrees, the wing incidence at the root is 5.3 degrees, with the wing tip incidence at 3.5 degrees (washout twisted into the wing). The stock engine down-thrust is 6.6 degrees.
The airfoil is flatbottomed with a thickness of 5%. I think that the large wing incidence is present because it is a slow flyer and it might cause problems when the airspeed in increased with load. The wing incidence will be fixed once things are glued together and will not be easy to change. My intuition hints that the wing incidence ought to be reduced by a couple of degrees to 3.3 at the root to 1.5 at the wingtip.
Reports from others suggest that the engine downthrust should be reduced to -3 degrees.
What advice do we have on this situation?
--Bill