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103,000+ materials, every value traceable to its source — MIL-HDBK-5J, DOI-linked papers, official compliance lists. Export solver-ready cards to 11 CAE formats.
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| 1 | ** MatWorld CAE Material Export — Abaqus (.inp) |
| 2 | ** Source: MIL-HDBK-5J · DOI 10.xxxx · Table 5.4.1.0(b) |
| 3 | ** Material: Ti-6Al-4V plate · Basis: A · Form: Plate |
| 4 | ** |
| 5 | *MATERIAL, NAME=Ti_6Al_4V_Plate |
| 6 | ** Orthotropic elastic card from L/LT/ST orientation data. |
| 7 | *ELASTIC, TYPE=ENGINEERING CONSTANTS |
| 8 | 1.14e+11, 1.10e+11, 1.07e+11, 0.342, 0.342, 0.342, 4.40e+10, 4.40e+10, |
| 9 | 4.40e+10 |
| 10 | *DENSITY |
| 11 | 4430., |
| 12 | *PLASTIC |
| 13 | 8.80e+08, 0.00 |
| 14 | 9.50e+08, 0.015 |
| 15 | 1.02e+09, 0.05 |
| 16 | *EXPANSION, TYPE=ISO |
| 17 | 8.6e-06, |
| 18 | *CONDUCTIVITY |
| 19 | 6.7, |
| 20 | ** ───────────────────────────────────────────────────────── |
| 21 | ** Fatigue + fracture data |
| 22 | ** Fracture toughness K_IC: 75 MPa·√m |
| 23 | ** S-N curve (cycles → stress), 5 points: |
| 24 | ** Source: MIL-HDBK-5J · Figure 5.4.1.1.8(a) |
| 25 | ** 1.0e+03, 8.5e+08 |
| 26 | ** 1.0e+04, 6.5e+08 |
| 27 | ** 1.0e+05, 5.2e+08 |
| 28 | ** 1.0e+06, 4.1e+08 |
| 29 | ** 1.0e+07, 3.2e+08 |
| 30 | ** ───────────────────────────────────────────────────────── |
Plus six more native formats
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CoCr, Ti-13Nb-13Zr, Nitinol, HA, bioglass, pyrolytic carbon.
Sources we cite
Click any property value in MatWorld to see the exact handbook page, figure, or paper it came from. Compliance results are checked against the official European and California registries — never guessed from element composition.
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