***
Generally speaking higher aspect ratio with either a fixed span or  area will 
equal a reduced wing chord. This will result in reduced reynolds  numbers 
which equals reduced performance for most all airfoils
***

Yes, but also .... what's happening (for a fixed wing span) is a  trade off 
between wing loading and induced drag. Re (at least for DLG chords and  up) is 
a variable but not the dominant one.

As you increase aspect ratio (reduce chord for a fixed wing span),  induced 
drag goes down but wing loading goes up. The wing loading will  eventually 
degrade your sink rate more than the aspect ratio improves it.  Although the 
wing 
weight scales with area, the total weight does not (fuselage,  tail surfaces, 
ancillary equipment). Re will hurt here as well (both Cd and Cl)  but it's 
primarily the loading (except perhaps at very small chords).

On  the other end, lower aspect ratio gives a lower wing loading but 
increased  induced drag (Cl^2/(Pi * AR).

In between there is an optimum - but it  will depend on the specific weight, 
planform limitations etc.
 
You can do this in a spreadsheet by using the induced drag formula, typical  
airfoil data (a flat plate data set is available from UIUC) and the needed Cl  
(at each velocity) from the lift equation. For a quick and dirty you can 
ignore  parasitic drag, or just use a constant term for the fuselage.
 
This has been covered several times in RCSD for DLG, 2M and open class  
simulations. 
 
Optimum for typical 2M construction is in the 9-11 AR range. For open it's  
typically in the 11 -15 AR range. Specifc results depend on airfoil and  
estimated final weights but these ranges are about right. DLG is more sensitive 
 but 
appears to optimize in the same range as 2M - probably due to the lighter  
weights of these ships. 
 
The absolute numbers may be off a bit since these calculations aren't well  
calibrated with real world flight data. But the trends are pretty  consistent.
 
Neat project with a nice result. A reasonably straight forward  simulation 
should emulate the general trend reported.
 
- Dave R
 
 
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