by Felix/FFDS » Fri Jun 27, 2003 10:40 am
control surfaces - ailerons/elevators/rudders - were subject to more stresses, especially at high speed/high G maneouvers. Before construction techniques improved, metal surfaces could buckle under the stress, leading to fatigue, cracks and possible disintegration in flight (not a good idea). Fabric surfaces provided for a certain "give" to the stresses.
As materials and construction techniques improved, fabric surfaces gave way to metal surfaces all over.
Felix/FFDS