Cmh17 Fiber Reference: 6.2.3.4.2(a)
011 to 014
CMH-17/MIL-HDBK-17-3F fiber and reinforcement reference tables. Includes typical fiber properties (carbon, glass, aramid, boron), nominal composite properties for various reinforcement types, fiber sizing/finish compatibility data, and general reference data from MIL-HDBK-17-3F Chapter 2 and CMH-17 Chapter 6.
| table id | row index | c1 | c2 | c3 | c4 | context | source page |
|---|---|---|---|---|---|---|---|
| 6.2.3.4.2(a) | 011 | TITANIUM shear stress – ksi MPa peel stress – ksi MPa | 0.061 0.419 -0.067 -0.465 | 0.338 2.33 -0.541 -3.73 | 2.27 15.64 -2.817 -19.43 | MIL-HDBK-17-3F Volume 3, Chapter 6 Structural Behavior of Joints TABLE 6.2.3.4.2(a) Generic mechanical properties of composites (Reference 6.2.3.4.2(a)). Unidirectional Lamina 0/90 Laminate Composite E L , E T , ν LT α L | 344 |
| 6.2.3.4.2(a) | 012 | STEEL shear stress – ksi MPa peel stress – ksi MPa peel stress – ksi MPa | 0.789 5.44 -0.914 -6.30 -3.54 -24.4 | 1.16 7.99 -2.17 -15.0 -5.82 -40.1 | 3.80 26.22 -5.52 -38.1 -6.47 -44.6 | MIL-HDBK-17-3F Volume 3, Chapter 6 Structural Behavior of Joints TABLE 6.2.3.4.2(a) Generic mechanical properties of composites (Reference 6.2.3.4.2(a)). Unidirectional Lamina 0/90 Laminate Composite E L , E T , ν LT α L | 344 |
| 6.2.3.4.2(a) | 013 | ALUMINUM shear stress – ksi MPa | 4.02 27.7 | 4.08 28.2 | 5.86 40.47 | MIL-HDBK-17-3F Volume 3, Chapter 6 Structural Behavior of Joints TABLE 6.2.3.4.2(a) Generic mechanical properties of composites (Reference 6.2.3.4.2(a)). Unidirectional Lamina 0/90 Laminate Composite E L , E T , ν LT α L | 344 |
| 6.2.3.4.2(a) | 014 | t -- 0.2 inch (5.08 mm); t adjusted for equal adherend stiffnesses; t = .01 inch (0.253 mm) i o b Adhesive properties: shear modulus -- 150 ksi (1.03 GPa) peel modulus -- 500 ksi (3.49 GPa) Cure temperature 250°F (121°C); Application temperature 75°F (24°C) | — | — | — | MIL-HDBK-17-3F Volume 3, Chapter 6 Structural Behavior of Joints TABLE 6.2.3.4.2(a) Generic mechanical properties of composites (Reference 6.2.3.4.2(a)). Unidirectional Lamina 0/90 Laminate Composite E L , E T , ν LT α L | 344 |
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