A challenge and a possible thread hijack (sorry). Forum owner feel free to slice this off into another thread if deemed appropriate.
This competition is an interesting challenge from a designer's point of view. The B-25 guys did the best so far apparently. Since we have plenty of clever guys on this board, an interesting exercise is how would you design a system to break the distance record (once AKT and his bad-ass Alaska posse wins it
this year)? Here's how I would do it...
The span is limited but not the chord. So
within reason you could increase the wing area a little as needed. Aspect ratio is all well and good when you are building a glider, but it appears to my non-degreed self that you want lifting area more than span in this situation.
Stability and control about the pitch axis seems to be a huge cause of spectacular failure in this competition. Ground effect also seems to be a primary factor in all the successful flights, from the B-25 to several others. The low launch height limits the available "power", so ground effect is a biggie.
So we might take a page from history and revisit the
un-successful efforts of Samuel Pierpont Langley's "aerodrome" It is shown here on its flugtag-like launch platform:
http://www.wright-brothers.org/History_ ... seboat.jpgIt is basically an equal tandem wing. The reason for this config. is that it puts two lifting surfaces with flugtag-legal span into ground effect, and provides a distance between the two wings to enable pitch control, by using the forward wing as a "canard" control surface. Pretty simple to move the pilot fore and aft to find the right CG to make this controllable.
So once you solve the problem Langley had in 1903 (torsional rigidity during catapult launch acceleration), you stand a good chance of a flyable, controllable aircraft. This was proved out when Glenn Curtiss, in a
bizarre development of his lawsuit with the Wright Bros., flew the Aerodrome over 3000 feet in ground effect, many times further than the Wright's aircraft original flight.
My hypothesis is that putting two equal span wings into ground effect would allow the longest achieved glide distance, for a span-limited aircraft having very limited energy from gravity. If this subject is of interest to people on this forum, we can go to the next step of how to maximize the available energy to achieve the longest flight.
There are several aero degrees and college professors and real-life engineer type folks lurking in these waters, so feel free to pipe up and disembowel my approach to shattering the flugtag distance record.