Hygrothermal expansion of Kevlar 49/epoxy and S2-glass/epoxy composites

Technical Report · Mon Nov 01 00:00:00 EST 1982

OSTI ID:6802126

Lo, S Y; Hahn, H T

Ply failure occurred during preconditioning at 75/sup 0/C of (0/90)/sub 2S/ S2-glass/epoxy and Kevlar 49/epoxy laminates. Wet specimens showed different thermal expansion beavior near and above the glass transition temperature. Various available theories can be used to predict the thermal expansion coefficients. Stress analysis showed that the compressive normal stress at the interface in Kevlar 49/epoxy after cure is very small compared with those in other composites. Significant and rapid changes in the transverse coefficient of thermal expansion occurs in the T/sub g/ region. The two-phase diffusion model is a good representation of the diffusion behavior. Desorption process reveals a higher diffusion coefficient than absorption. S2-glass/epoxy was found to be unstable under the conditions applied, with cracking and losses during desorption. Maximum moisture contents were approx. 0.31% at 75/sup 0/C/75% RH and approx. 0.412% at 75/sup 0/C/water. The composite swelled transversely up to about 0.11 and 0.16%. Kevlar 49/epoxy was more stable than S2-glass/epoxy; max moisture contents were approx. 2.47% at 75/sup 0/C/75% RH and approx. 5.5% at 75/sup 0/C/water. The composite swelled transversely up to 1.0 and 2.23%. Results indicate that Kevlar 49 fibers swell radially. Relation between swelling strain and moisture content undergoes hysteresis during moisture cycling. Relation between swelling strain and moisture concentration is fairly linear for S2-glass/epoxy, Kevlar 49/epoxy and AS 3501/5 graphite/epoxy and only weakly depends on the material system. The equilibrium moisture content in (+-45)/sub 2S/ laminate is higher than in unidirectional lamina. The equilibrium thickness swelling strain can be predicted by laminated plate theory.

• Research Organization: Washington Univ., St. Louis, MO (USA)
• DOE Contract Number: W-7405-ENG-48
• OSTI ID: 6802126
• Report Number(s): UCRL-15517; ON: DE83006567
• Country of Publication: United States
• Language: English

Related Subjects

36 MATERIALS SCIENCE
COMPOSITE MATERIALS
SWELLING
REINFORCED PLASTICS
ARAMIDS
CRACKS
DESORPTION
DIFFUSION
EPOXIDES
FAILURES
FINITE ELEMENT METHOD
GLASS
MOISTURE
STABILITY
STRESS ANALYSIS
THERMAL EXPANSION
EXPANSION
MATERIALS
NUMERICAL SOLUTION
ORGANIC COMPOUNDS
ORGANIC OXYGEN COMPOUNDS
PETROCHEMICALS
PETROLEUM PRODUCTS
PLASTICS
REINFORCED MATERIALS
SYNTHETIC MATERIALS
360305* - Composite Materials- Corrosion
Erosion
& Degradation- (-1987)