I am dubbing it 'XS1' (Experimental Single-seat #1). What is shown below is the layout for the tubing that will form the fuselage. I am going with an old-school style of construction after seeing how rugged and cheap this technique can be on the WACOs and Great Lakes. Thus the fuselage frame will be steel tubing (probably 4130 Chromoly), tube sizes are something I am currently investigating.
This airplane will be a single seat tail dragger with a single low wing. The engine currently being used for reference is the Lycoming IO-360. My ultimate goal is to produce an aircraft reminiscent of a early WW2 era fighter with either an open or closed cockpit (or semi-enclosed like many early/pre WW2 fighters).
Skin will thus be a mix of aluminum sheet and fabric with some sheet metal and wooden bulkheads and fuselage formers like the WACO YMF5 and Great Lakes.
I am planing on making the seat in a fairly reclined position (shooting for ~20degrees) to give that 'go-fast' feel as well as for comfort. Avionics will be the usual stuff you see in small single seaters of today.

Please note, I have done 0 stress analysis thus far; this represents the very beginning of my project. I hope to make this my senior design project in school as well. So periodically I will post screen shots of progress as the design grows.
engine:
http://www.lycoming.textron.com/engines ... Insert.pdf
tube sizing being investigated:
http://www.cartesiantube.com/documents/ ... f#view=Fit
Serious suggestions are welcome!
Tailwinds,
Adam