(Snip)
The various knuckle-type hinge deals are a different way to go about it. Al's car-hood experiments showed the "blended-flap" type of flap and knuckle hinge (like Keith Trostle's NATs winner), to everyone's surprise, gave less lift than a conventional hinge and flap. That may have been for the reason Al thought -that the upper surface discontinuity caused separation. His solution (much like Igor's) was to move the high point aft to that the fixed and moving sections faired in better with the very large deflections used at the time.
(Snip)
Brett
Interesting question. Interesting comments. And a pertinent comment about Al's "car hood" experiments. All relevant.
First. All of my stunt models use the recessed hinge line for the flaps, elevators and on my rudders. (I use a variation of the Rabe Rudder to offset gyroscopic recession, but that is another subject.) I feel that my stunt ships over the years have turned as well as most.
Yes, Al's experiments showed the flap as part of the airfoil with the recessed hinge line based on the airfoil on my Ta 152 that won the '70 Nats did not produce as much lift as the airfoils that he developed for his Super Semi Scale Stunt Ships (S
5). His experiment was not flawed, but the test sample he made was and I will try to explain.
On that test, Al offset the hinge line behind the radius of the flap leading edge so that when the surface starts to deflect, that leading edge starts to seal the gap between the flap. The result was that the flap LE slightly raises above the surface of the wing TE. This acts as a span wise spoiler to the airflow over that portion of the wing. In all probability, that airflow is already turbulent before it reaches the flap. But when the airflow encounters that spoiler, it will separate, thus reducing the effectiveness of the flaps. As Brett mentioned in his paragraph above, this "surface discontinuity" may have caused separation. I know for a fact that any kind of spoiler at that wing/flap area absolutely reduces lift. I could go into a long explanation about how I know this for a fact, but just suffice it to say here that when I use tape to seal the hinge lines (even on these recessed hinge line configurations - yes, it can be done), the method of applying that tape will sometimes result in a slight ridge forming at the hinge line (due to oil causing the tape adhesive to not properly stick to the surface - another long explanation), that the turning ability of my ships is significantly reduced. So, in other words, Al's tests, impressive as they were, did not give a true measure of the effectiveness of that flap hinging arrangement if the hinge line would have been properly placed.
What I do with all of my stunt ships is to place the hinge line slightly in front of the LE radius (even works on tapered thickness flaps/elevators - another long story) so that the flap (elevator) LE edges starts to recede from the surface of the wing (stabilizer) TE. This give the effect of having the flap (elevator) thickness being slightly less than the LE preceding it. And, in my opinion, as well as others, having control surfaces slightly thinner that the wing (stabilizer) TE is desirable because the models seem less sensitive around neutral to have a better groove with little or no effect on turning ability/responsiveness.
So, my recommendation to whoever wants to play with this business of recessed hinge lines on flaps and elevators, do so. But I would strongly recommend the four following points.
1. Place the pivot point slightly ahead of the flap and elevator hinge lines. I have found that 1/32" is sufficient for the difference on a full size stunt ship.
2. Contour the TE of the wing/stabilizer to the contour of the flap and elevator LE to minimize any gap throughout the flap elevator movembent. In this thread, this is called fairings at the TE.
3. There is a way to tape these hinge lines. I have found on all of my stunt ships for the past 20 years or more that it is effective to tape the elevators, less effective to tape the flaps with these kind of hinge lines. When fabricating the TE fairing, allowances should be made to be able to tape the hinge line. For those that are interested, I will explain.
4. Keep in mind that when the hinge line is recessed into the flap and elevator leading edges, that the "effective area" of the flaps and elevators is being reduced by the distance of that hinge line to the flap and elevator hinge lines. The chord of the flap and elevators should be increased by that amount to maintain the same "effective area". (What I am calling "effective area" is the area behind the hinge lines.)
Now, for a disclaimer:
I am in no way a golden arm in the world of serious competition stunt. Over the years, my airplanes have performed well in competition using this recessed hinge line idea and have had adequate turning ability, and some observers have commented after flying my models that they turn better than most. My designs often have wing flaps that are as munch as 1" thick at the root tapering to 5/8" at the tip with an elevator that is almost 3/4" thick at the root to 1/2" at the tip.
What I have written here is not to argue or disagree with anyone. Instead, what I have written is based on my observations and experiments over more than a few years.
(That Focke Wulf that won the 70 Nats was limited in its turning ability because it had 15% flaps and a 15% tail which was not uncommon in the designs from that period. By the way, another Focke Wulf, same design, from the RSM kit won the Classic event at the 2008 Nats.)
Keith