By Steven L. Donaldson, Daniel B. Miracle
ASM instruction manual, quantity 21: Composites presents a entire, useful, and trustworthy resource of technical wisdom, engineering facts and aiding info for composite fabrics. This guide is meant to be a source quantity for nonspecialists who're drawn to gaining a realistic operating wisdom of the services and purposes of composite fabrics. insurance emphasizes well-qualified and priceless info for fabrics that may be produced in amounts and product varieties of engineering importance.
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Additional resources for ASM Handbook Composites Volume 21
References cited in this section 2. P. G. D. Karmarkar, Silicon Carbide Reinforced Aluminum—A Formable Composite, JOM, Vol 33 (No. 9), 1981, p 12–17 3. G. Fishman, Office of Naval Research, private communication, 1997 4. N. , Norwalk, CT, 2000 General Use Considerations General Characteristics. First and foremost, composites are engineered materials that have been designed to provide significantly higher specific stiffness and specific strength (stiffness or strength divided by material density)—that is, higher structural efficiency—relative to previously available structural materials.
In addition, existing aerospace structural alloys, such as those based on aluminum, were subject to corrosion and fatigue damage, and OMCs provided an approach to overcome these issues. By the end of the war, glass-fiberreinforced plastics had been used successfully in filament-wound rocket motors and demonstrated in various other prototype structural aircraft applications. These materials were put into broader use in the 1950s and provided important improvements in structural response and corrosion resistance.
S. tactical fighter aircraft, the F-22. Over 24% of the F-22 structure is OMCs. The B-2 bomber, shown in Fig. 2, is constructed using an even higher percentage of composites, as are current helicopter and vertical lift designs. For example, the tilt- rotor V-22 Osprey is over 41% composite materials. The upper-use temperature of PMCs has also increased dramatically: early epoxies were considered useable (for extended periods) up to 121 °C (250 °F). Current generation polymers, such as bismaleimides, have increased that limit to around 204 °C (400 °F), and the use of polyimide-matrix composites has extended the range to 288 °C (550 °F).