- #1
Murmur79
- 10
- 0
AFAIK, the wood used for aircraft structures should have a specific stiffness, that is specific Young's modulus and bending strength, somewhat higher than aluminium (see attached image).
If that is the case, why wood aircrafts are generally more subject to aeroelastic effects compared to aluminium ones?
If that is the case, why wood aircrafts are generally more subject to aeroelastic effects compared to aluminium ones?