Shape memory polymer filled honeycomb model and experimental validation
Creators
- 1. University of Dayton Research Institute, 300 College Park, Dayton, OH 45469-0013 (United States)
- 2. Air Force Research Laboratory, Wright-Patterson Air Force Base, OH 45433 (United States)
Description
An analytical model predicting the in-plane Young's and shear moduli of a shape memory polymer filled honeycomb composite is presented. By modeling the composite as a series of rigidly attached beams, the mechanical advantage of the load distributed on each beam by the infill is accounted for. The model is compared to currently available analytical models as well as experimental data. The model correlates extremely well with experimental data for empty honeycomb and when the polymer is above its glass transition temperature. Below the glass transition temperature, rule of mixtures is shown to be more accurate as bending is no longer the dominant mode of deformation. The model is also derived for directions other than the typical x and y allowing interpolation of the stiffness of the composite in any direction. (paper)
Availability note (English)
Available from http://dx.doi.org/10.1088/0964-1726/24/2/025019Additional details
Identifiers
Publishing Information
- Journal Title
- Smart Materials and Structures (Print)
- Journal Volume
- 24
- Journal Issue
- 2
- Journal Page Range
- [11 p.]
- ISSN
- 0964-1726
INIS
- Country of Publication
- United Kingdom
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 47054295
- Subject category
- S36: MATERIALS SCIENCE;
- Resource subtype / Literary indicator
- Numerical Data
- Descriptors DEI
- BENDING; EXPERIMENT RESULTS; EXPERIMENTAL DATA; FLEXIBILITY; GLASS; HONEYCOMB STRUCTURES; POLYMERS; RODS; SHAPE MEMORY EFFECT; SHEAR; TRANSITION TEMPERATURE; YOUNG MODULUS
- Descriptors DEC
- DATA; DEFORMATION; INFORMATION; MECHANICAL PROPERTIES; MECHANICAL STRUCTURES; NUMERICAL DATA; PHYSICAL PROPERTIES; TENSILE PROPERTIES; THERMODYNAMIC PROPERTIES