Experiments on Pulse Propagation in an Obliquely Laminated Composite.
Abstract
Experimental results are presented for the linear elastic dynamic response of periodically laminated composites. A shock tube-capacitive transducer technique is used to determine the rear surface velocity history of three laminated samples that have different lamination angles and are subjected to a step pressure loading. Viscosity effects are discussed, and comparisons are made with predictions based on previous theoretical work. (Author-PL)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 31, 1974
- Accession Number
- AD0777577
Entities
People
- Charles Sve
- Seichi Okubo
Organizations
- The Aerospace Corporation