On Friday 18 February 2005 17.12, [EMAIL PROTECTED] wrote:
> 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.
>

I think Martin Simons "Model Airplane Aerodynamics" is a good source for
info about this, not least appendix #1!

A practical, high AR wing, is by default heavier (if having the same area), 
than a low AR wing, which makes the gain with a high aspect wing smaller 
than expected, even though it has lower drag. Also, when talking constant 
area, and small models, the lower efficiency of small chord wings comes into 
effect. Also mechanical matters affect the calculations, as narrow wings
are more flutter-prone than low AR wings!

Thus, as we are talking equal wing area, short wings are light, affecting 
minimal sink, while good glide ratio, equals low L/D, but the longer they are 
the faster they have to fly, to maintain good Reynold's numbers!

If I remember correctly, your wings were all balsa sheet, thus approximately
the same weight no matter what Aspect Ratio they have. The reason that
AR about 7 are optimum, is that longer wings have too small AR to be 
efficient, while shorter have too big induced drag!

In the real world high aspect ratio wings are perfect, as long as you can 
build a strong enough wing, but they will be default be heavy! 

But if you have a motor the calculation gets more difficult, as a lot
of induced drag during take-off and landing, due to short span,
can be compensated by brute power. At cruise speed and straight flight
long wings are not that helpful, unless the engine can be throttled back
efficiently!

So a motorglider has very low useful load, but excellent fuel economics!

Good luck,

Tord
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