
I quickly built three half-size concept models. They all show promise. Which one do you like?
Pickerel Prototype #1
As reported earlier, the first prototype came out very tail heavy. Even if I had mounted the motor on the nose, the center of gravity would have been too far back. Back to the drawing board!
Rethinking the Design
Why was it so tail heavy? First, flying wing (tailless) designs are often flown tail heavy out of ignorance. If you use the common rule of thumb of putting the CG at 25% of the chord, you will be flying it tail heavy. Because there is no separate tail, the equivalent position for a tailless is 15% of the chord.
The combination of a relatively high taper ratio (0.5) along with a high sweep angle was not good. This put most of the lift production in the center with little wing area in the tips to balance things out.
Flying Wing Spreadsheet
I put together a simple spreadsheet to help me understand all the variables that control how a flying wing will fly. Supporting up to three panels per wing half led to a large number of intermediate calculations. The rows containing these calculations are hidden. Only manually edit the rows colored in blue. All the rest are computed results.
Crescent Wing
Looking for a simple design that did not have much wing taper, I came up with a crescent-shaped wing. It is basically just a semi-circle.
I ran into two problems right away. First, this shape is harder to analyze. It is not easy to enter its numbers into my spreadsheet. Second, despite its simplicity, it was not easy to build. I had to cut it out freehand. No, I am not very good at cutting accurate curved shapes. Most model airplane builders are not, either.
The half-scale free flight prototype flew fine. It had reasonable stability along all three axes.
Joined Wing
A design idea that has gotten a lot of attention with full-scale airplane designers during the last ten years is the joined wing. Another very hot concept is raked wing tips. I decided to combine the two into a futuristic Pickerel concept design. The front wing sweep angle is 45 degrees.
Out of the three half-scale prototypes, this is the one that proved to be directionally unstable. Whenever I launched it, it was just as likely to curve to the left as to the right.
However, after I added a vertical stabilizer it proved to be the most stable of the three. The design shows a lot of promise.
I ran into two problems with this one. First, the shape of the gap between the wings makes fitting the motor a challenge. I really want the motor to be as close to the nose as possible, and this design does not let me do that.
Second, the design is pretty wide. It is hard to build from a single sheet of foamboard.
Diamond Wing
Looking to fix the problems with the joined wing prototype, I decreased the amount of wing sweep and got rid of the wing extensions. That led to the diamond wing design. Here the sweep of the front wing is down to 30 degrees.
The sweep of the front wing is a little more than the wing in the rear. Surprisingly, this design proved to be directionally stable without a vertical stabilizer.
This shape is very strong and fits in well within a sheet of foamboard. It was also very easy to build.
Feedback
I wonder if the best design would be a joined wing using 30 degrees of sweep. I’ll bet it would look and fly great. I do not think it would fit into a single sheet of foamboard, though.
What do you think? Which one do you like better?
Pickerel article index and discussion thread in forums.











Carlos: I believe that any of your three new Pickerel configurations will fly just great. Whereas the diamond wing may very well be stable directionally as a glider, with a propeller-driven electric motor you will probably need some vertical tail for spiral stability. As to CG location, as you have stated 25% chord is fine for a rectangle or square–but the rule of thumb is 25% of MAC which is different for other shapes. For these three new configurations, since you have the front and rear wing with the hole in the middle it is necessary to determine the 25% MAC for each wing. Then you determine the wing area for each wing with its 25% MAC marked and put the CG between the two based on ratio of the areas. For an example, if the distance between the two CG’s is 10″, and the area of the forward wing is say 100 square inches and the area of the aft wing is 100 square inches, then the CG would be half-way (or 5″ aft of the forward wing’s CG). It’s like a teeter-totter arrangement. The CG is the pivot for the teeter-totter. Another example would be the 10″ between the two wings’ 25% CG’s with the front wing having say 100 square inches of area and the aft wing having only 50 square inches. The ratio of the two areas is two; therefore the CG would be 3.33″ aft of the forward wing’s 25% MAC.
Hope this clarifies my understanding of CG’s. The CG if moved forward of the combined 25% CG’s will need more decalage (angular difference between the forward and the aft wing (i.e., up elevator, not different from convential wing and horizontal tail. There is also the consideration of downwash on the aft wing at certain angles of attack with causes a nose-up pitching moment–all of which can be trimmed out with the elevator on the aft wing. Cheers. Don Larsen
I am currently pursuing a joined wing configuration with 30 degrees of sweep instead of 45. I loved the look of the joined wing prototype with the raked wing tips. The fact that it flew the best of the three sealed the deal.
The stability rule is a little different than what you stated. The assumption is that the aerodynamic center (AC) is at 25% of the MAC. It is never exactly at this point, but is almost always close. The rule then is to be about 10% ahead of the MAC.
The thing is, in a conventional configuration airplane the horizontal tail is about 10% of the area of the wing. That pushes the AC about 10% back towards the tail. When you go 10% forward for stability, you end up back at exactly the same 25% MAC but that is purely a coincidence.
In a flying wing, the same rule applies. 10% forward of the AC, which is assumed to be at 25% of the MAC. But since there is no tail, you end up at 15% of the MAC.
Your explanation of the method for accounting for multiple wings is correct. In fact, that is exactly the same method I used in the spreadsheet to account for the multiple wing panels. It is a weighed average.
In joined wing aircraft the rear wing is normally mounted high, to avoid the downwash from the front. I won’t probably have that, though the prototype flew just fine the way it was.
Carlos:
Thank you for your cogent comments on my Pickerel CG thoughts. It is interesting that attacking the CG from two different perspectives results in about the same conclusion for a starting CG location, coincidence or not. Airfoil pitching moments also influence the optimum CG location for any particular configuration. Of course, the proof of the pudding is in the flying–which generally requires some fine tuning. Your 30 degree sweep joined wing sounds exciting and I am inspired to design one myself. I like your Depron reinforcement on the underside of the front wing’s leading edge–as that allows for some LE shaping, if desired, and makes the wing more rigid. Your website, for me, is the best there is and its a wonderful “addiction”. Keep up the great work! Respectfully, Don Larsen
Yes, the specific airfoil makes a difference as far as pitch stability.
I am being very honest in showing my typical design approach, with this airplane being the example. I try and maintain a healthy balance between theory and practice, using each to best advantage.
Yesterday I built a half scale prototype of my 30 degree joined wing design. After some fine tuning, it is now flying beautifully. I am very excited to build and fly a full scale version!
The reinforcement is on top of the wing, not the bottom. I should record a video about why I am using a regular airfoil on a flying wing.
Finally, thank you for the very kind words. I take all the feedback I get very seriously, and I appreciate you taking the time to comment on my design. If there is something that you would like to see on my website, let me know!