I've unfortunately come to the conclusion that the combination of this plane and me as a pilot just won't really work. It's too small and too fast for me to manage. I've gotten it up to 126 mph, but at that point it's a tiny dot that I can't really keep track of and I lost control and crashed pretty quickly. I think it could go faster, but not with me at the controls. Launching it is also a bit of a lottery - it's about a 50-50 chance on if it gets airborne or smashes into the ground. Ultimately, because I designed it so fast, and especially because it's so small to make the print time as short as possible, I think I compromised it's flyability for the sake of speed.
I still want to go faster however, and I like the basic design, so think I'm going to split this into two longer term projects.
One will be a boundary layer ingesting wing designed to use a 64mm fan instead of the 50mm fan in this design. It will be designed for flight time more than speed in an effort to keep the stall speed more reasonable and because I want to get more of sense of how this kind of design flies without it being a dot I can't see most of the time. The wingspan is 1200mm vs. the 500mm wingspan of the original speed plane. It uses the MH 45 flying wing airfoil which also makes the wing more efficient than that of the original plane, although it's so much bigger that it still won't go anywhere near as fast.
The other design will be meant to go fast. It's much more conventional and uses 2 of the 50mm EDF units instead of the single one I used in the original. This gives it enough power to carry a larger wing and more importantly, retracts, which will make launching a lot simpler. I'm currently still working on optimizing it to reduce drag, but this is the current design. My current prediction is 140-160 mph for the top speed, but I'm hoping to maybe get a bit faster still.
At the heart of this design is a new airfoil I designed to get the performance I'm looking for. It's a laminar flow airfoil designed for Reynolds numbers between 300,000 and 1,500,000 and the XFoil and CFD predictions have it outperforming even the amazing MH27 and MH 16 pylon racer airfoils, especially at lower Reynolds numbers. It is substantially more efficient than the original NACA airfoil I selected for the smaller flying wing which allows a thicker larger wing (to fit gear) and a lower stall speed without a significant penalty in terms of top speed.
As a comparison with the MH 27 airfoil, here are some plots of the performance. The MH 27 airfoil is in pink, and my airfoil in dark blue. You can see the difference between the two is not all that substantial. My airfoil has less about 15% less drag at a Reynolds number of 1,500,000, and at lower angles of attack at the cost of a smaller drag bucket. This increases to 30% less drag at a Reynolds number of 300,000 Since I'm not pylon racing, I don't really need to worry about higher drag above a 4g turn, since I won't really be turning that hard at high speeds anyways. XFoil didn't converge for my airfoil at higher AOAs, but from CFD, the max lift coefficient is almost exactly the same. The pitching moment is also very comparable which means I'm not adding back in trim drag.