An increasingly important part of the design of skin-stringer systems, such as those found in flight vehicles, is the ability to reduce surface vibration levels when they are subjected to the dynamic loads of jet, or propeller noise. One common method of reducing the response of these structures is by layered construction using viscoelastic materials. Thus analytical methods to describe such systems are essential.
Response of stiffened sandwich panels
Conference on Structures, Structural Dynamics and Materials ; 1981 ; Atlanta, GA
01.01.1981
Sonstige
Keine Angabe
Englisch
Response of stiffened sandwich panels
AIAA | 1981
|Study of thermal-expansion-molded, graphite-epoxy hat-stiffened sandwich panels
Tema Archiv | 1991
|