Doug, read this...
http://home.hiwaay.net/~sbuc/journal/smart.html
Twice.
Here at VAF we embrace the axiom "There are no dumb questions" because the goal is to get everyone in the air safely. However, the question can tell us a lot.
The number one error made by builders new to fiberglass work is failure to conceptualize...to fully grasp what they want to accomplish, and then work out all the steps to get there, in advance, in detail, starting from zero. Instead they start hacking up cloth and slapping it on willy-nilly, use too much epoxy, and wind up with a lumpy mass that looks like a cross between a meteorite and a hairball. For them, the next step is a load of bondo, or some other "easy" filler...when really good composite work takes almost no filler at all.
Conceptualizing means building the
imaginary part to completion, from zero. When you ask "How much glass cloth?" you're telling me that you have not conceptualized....as the first steps are to get some dimensions, and decide how may plies the layup will require to get the finished
thickness necessary for the desired
stiffness. The answer to your question is found in Area x number of plies. Rough thickness per ply is right there on the order page in the catalog.
How much total thickness is desired for a finished part? Evaluate its use. Is it structural, or aerodynamic, or merely cosmetic? Does it get a lot of human abuse, or does it have a gentle life? Is it screwed on, or bonded evenly? You get to make these decisions based on what you conceptualize as a result, as it's a custom built airplane. If fabric choice, number of plies, and ply orientation are critical, the information will be in the plans...as it is with real composite airplanes.
I beg your indulgence....better to teach
how to fish....