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Q: Are canards allowed? I have noticed some of the kits/plans call for a CG location aft of the center of lift, which would load the stabilizer as a lifting wing.
A: (2-2-10) Canards are allowed.
Q: Does the horizontal stab have to be aft of the main wing? At what point does this qualify as a Biplane?
A: (2-2-10) As long as the wing and stabilizer are in conformation with the specified dimensions, the airplane is not a biplane. The stabilizer does not have to be aft of the wing. If your question arises because the stabilizer has no maximum chord specified, it would be possible to have a stabilizer with a greater area than the wing. Because of that, this question should be deferred to the National Science Olympiad Rules Clarification process. In any case, only one wing and one stabilizer is allowed. That is, if there are 2 stabilizers and one wing or visa-versa, it would be a biplane.
Q: How wide can a piece of balsa wing structure be before it starts being considered a solid wing? Could you drill some holes in a solid wood wing, cover it with tissue, and then pass inspection?
A: (2-2-10) The specification for no "solid balsa wing or tail assemblies" may also need clarification by the National SO. However, to my way of thinking, just taking a solid sheet of balsa and cutting holes for lightening is not an assembly. Assembly means taking more than two separate pieces and joining them. For a wing with, for example a 10- cm chord, an assembly with LE and TE each 4cm wide joined by 2 cm long ribs would not be disallowed.
Q: Could we really use a formed carbon wing? I would hope no one would, but is this allowable under the rules as they are written?
A: (2-2-10) A formed carbon wing may be used as long as there are no pre-glued assemblies.
Q: Does the weight for the airframe include the prop & mount, or does that go with the rubberband weight?
A: (2-2-10) The airframe includes everything but the rubber motor. The propeller assembly is part of the airplane. The propeller assembly is not part of the rubber motor. (kids get confused by this sometimes).
Q: Are the span limits as projected to a flat surface below, or as measured from center (in other words, could you use dihedral to have an effectively longer wing)?
A: (2-2-10) The span for wing and stabilizer is the projected span. Span is measured on the assembled airplane. it is common for the pre-dihedral wing and stab to exceed the spec. Be careful that the propeller diameter does not exceed 20 cm as measured for all axis thru the center, not just on the centerline.
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