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Ernest Christley wrote:
Most of the fabric covered aiplanes I've seen didn't seem that hard. That is, you could walk up to them and push the fabric in with your hand. The way I understand the fabric process, it is basically a composite structure. You have a nylon cloth with a paint "epoxy". You have a cloth material coated with a doping silver compound to reinforce the material and make it taut, on top of which paint is applied. The former does not penatrate the material but is on one side. Could a much stronger and lighter covering be made by wetting out some 2.5oz glass cloth on plastic, waiting till it's tacky and then wrapping it around the airframe? The epoxy would be much lighter than paint, and fiberglass cloth is MUCH stronger than nylon. Keep in mind that fabric covered structures are not Load-bearing in the structural sense of the term. The fabric is there to keep the aerodynamic shape and provide an area for the pressure to act on. It is not a stressed skin structure in that the fabric takes pressure loading, especially on the wings, but does not contribute to the strength of the underlying framework as in metal skined designs. As such, the extra strength is not really required on existing fabric covered structures. You could maybe argue for a weight saving factor in the days of lead based paints, but now... There is the advantage of better UV resistance and not cracking or pealing over the lifetime. I've seen some places where builders used composites in place of fabric, and it seemed that they all aimed for a multlayer, stiff panel, putting the weight far above the original. I just don't understand why? This is where there is some skin loading required. Stressed skin designs can make the use of very thin aerofoil sections possible by taking some of the load off the spars and ribs making for lighter and stronger structures. |
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