Cmh17 Fiber Reference: 6.2.3.4.2(a)

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.

Aerospace Engineeringtable_id: 6.2.3.4.2(a)3 rows
table idrow indexc1c2c3c4c5c6c7c8contextsource page
6.2.3.4.2(a)001Unidirectional Lamina0/90 LaminateMIL-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 L344
6.2.3.4.2(a)002CompositeE , L Msi (GPa)E , T Msi (GPa)ν LTα L 10-6/F° (10-6/C°)α T 10-6/F° (10-6/C°)E x Msi (GPa)α x 10-6/F° (10-6/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 L344
6.2.3.4.2(a)003Boron/ epoxy29.1 (201)2.91 (20.1)0.176.50 (11.7)16.9 (30.4)16.5 (114)4.8 (8.6)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 L344

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