GTBL042-App-B GTBL042-Callister-v3 September 21, 2007 20:24
818 • Appendix B / Properties of Selected Engineering Materials
Table B.6 (Continued)
Coefficient of
Thermal Expansion
Material 10 −^6 (◦C)−^110 −^6 (◦F)−^1
FIBER MATERIALS
Aramid (Kevlar 49)
- Longitudinal direction –2.0 –1.1
- Transverse direction 60 33
Carbon (PAN precursor) - Standard modulus
Longitudinal direction –0.6 –0.3
Transverse direction 10.0 5.6 - Intermediate modulus
Longitudinal direction –0.6 –0.3 - High modulus
Longitudinal direction –0.5 –0.28
Transverse direction 7.0 3.9
E-glass 5.0 2.8
COMPOSITE MATERIALS
Aramid fibers-epoxy matrix
(Vf=0.6) - Longitudinal direction –4.0 –2.2
- Transverse direction 70 40
High-modulus carbon fibers-epoxy matrix
(Vf=0.6) - Longitudinal direction –0.5 –0.3
- Transverse direction 32 18
E-glass fibers-epoxy matrix (Vf=0.6) - Longitudinal direction 6.6 3.7
- Transverse direction 30 16.7
Wood - Douglas fir (12% moisture)
Parallel to grain 3.8–5.1 2.2–2.8
Perpendicular to grain 25.4–33.8 14.1–18.8 - Red oak (12% moisture)
Parallel to grain 4.6–5.9 2.6–3.3
Perpendicular to grain 30.6–39.1 17.0–21.7
Sources:ASM Handbooks,Volumes 1 and 2, Engineered Materials Handbooks,Volumes 1
and 4, Metals Handbook: Properties and Selection: Nonferrous Alloys and Pure Metals,
Vol. 2, 9th edition, andAdvanced Materials & Processes,Vol. 146, No. 4, ASM International,
Materials Park, OH;Modern Plastics Encyclopedia ‘96,The McGraw-Hill Companies,
New York, NY; R. F. Floral and S. T. Peters, “Composite Structures and Technologies,”
tutorial notes, 1989; and manufacturers’ technical data sheets.