Mechanical characteristics of composite structures are influenced not only by the geometrical and physical properties of the materials used but also by the many parameters characterizing the manufacturing processes such as temperatures and pressures in the polymerization cycle. Typical sandwich structures with carbon fiber reinforced plastics skins for aerospace applications have been manufactured with different process parameters in order to verify the induced changes in the modal parameters. Frequencies mode shapes and modal damping have been retrieved by using both Frequency Response Functions and Electronic Speckle Pattern Interferometry. Specimens have been tested in the free configuration by supporting the composite sandwich panels on soft material.
|Pages (from-to)||1311 - 1317|
|Number of pages||7|
|Journal||Proceedings of the International Modal Analysis Conference - IMAC|
|Publication status||Published - 2001|
All Science Journal Classification (ASJC) codes
Caponero, M. A., Ivagnes, M., Lecci, U., Paolozzi, A., & Santoli, F. (2001). Mechanical characterization of aerospace sandwich panels by speckle interferometry. Proceedings of the International Modal Analysis Conference - IMAC, 2, 1311 - 1317.