Wacobipe
100cc
I have the books written by Dave Scott of 1st US R/C Flight School, and I have also read an article by him recently in Model Airplane News (I think) where he references this idea and I am curious what everyone else thinks about this:
In these resources Dave proposes the following 2 things to improve aerobatic aircraft performance: A thicker control surface than the flying surface it is attached to (Aileron thicker than wing) and rounding the leading edges of control surfaces. I have attached scans of 2 pages of Sport Aerobatics written by Dave for reference but Let me explain in more detail.
First, Dave says that essentially all modern aerobatic full scale aircraft have thicker control surfaces than the flying surface they attach to (the LE of the aileron is thicker that the TE of the wing for example). The purpose of this is to push the control surface out beyond the turbulent air layer and into the smooth air beyond it. This provides much more precise control and also control at lower airs speeds.
Second, he suggests that a control surface leading edge should be round (not beveled as is the norm in the hobby). This round leading edge of a control surface should be attached to a trailing edge of the flying surface that is squared off, and not beveled or rounded (see images). To clarify let's consider an aileron. The aileron would attach to a squared off rear edge of the wing, and the aileron would have a rounded leading edge. By doing so, Dave says that turbulence over the control surface is reduced providing for more precice control.
Combined, these 2 design considerations improve the correlation between radio inputs and airplane reaction, allow for lower minimum controllable airspeeds, aircraft response is improved in aerobatics (especially on windy days and close to the ground), and the potential for flutter is greatly reduced (he claims sealing the gaps becomes unnecessary).
I am curious what everyone here thinks about these concepts so please throw your 2 cents into the conversation!
20068=12905-Scan 1.jpg
20068=12904-Scan 2.jpg
In these resources Dave proposes the following 2 things to improve aerobatic aircraft performance: A thicker control surface than the flying surface it is attached to (Aileron thicker than wing) and rounding the leading edges of control surfaces. I have attached scans of 2 pages of Sport Aerobatics written by Dave for reference but Let me explain in more detail.
First, Dave says that essentially all modern aerobatic full scale aircraft have thicker control surfaces than the flying surface they attach to (the LE of the aileron is thicker that the TE of the wing for example). The purpose of this is to push the control surface out beyond the turbulent air layer and into the smooth air beyond it. This provides much more precise control and also control at lower airs speeds.
Second, he suggests that a control surface leading edge should be round (not beveled as is the norm in the hobby). This round leading edge of a control surface should be attached to a trailing edge of the flying surface that is squared off, and not beveled or rounded (see images). To clarify let's consider an aileron. The aileron would attach to a squared off rear edge of the wing, and the aileron would have a rounded leading edge. By doing so, Dave says that turbulence over the control surface is reduced providing for more precice control.
Combined, these 2 design considerations improve the correlation between radio inputs and airplane reaction, allow for lower minimum controllable airspeeds, aircraft response is improved in aerobatics (especially on windy days and close to the ground), and the potential for flutter is greatly reduced (he claims sealing the gaps becomes unnecessary).
I am curious what everyone here thinks about these concepts so please throw your 2 cents into the conversation!
20068=12905-Scan 1.jpg
20068=12904-Scan 2.jpg