Optimization of constrained viscoelastic damping treatments for passive vibration control
- 13 April 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Preliminary Design of Composite Wings for Buckling, Strength, and Displacement ConstraintsJournal of Aircraft, 1979