Certainly would be better to laminate IF you're using wood. But it's still got a long road ahead. Aluminum still has a higher strength/weight ratio which is ev

Certainly would be better to laminate IF you're using wood. But it's still got a long road ahead. Aluminum still has a higher strength/weight ratio which is everything in aero. Also, I'm not finding any information on cyclic strain behavior. Dimensional stability is only part of that. Edit: There could be room for this in experimental aircraft. Once we tease out all the failure modes and properly characterize cyclic behaviorof course.