Aeroelastic stability characteristics of a composite swept wing withtip weights for an unrestrained vehicle
LOTTATI, I.
Journal of Aircraft ; 24 , 11 ; 793-802
1987
Article (Journal)
Electronic Resource
English
Swept composite wing aeroelastic divergence experiments
AIAA | 1982
|Aeroelastic divergence of unrestrained vehicles
AIAA | 1981
|