In its most primitive form a composite material consists of two dissimilar materials, one being the matrix and the other the reinforcement. These materials are selected so as to mechanically compliment one another whilst neutralising their deficiencies. The reinforcement may have high strength in tension, but little resistance to bending and compressive forces, the matrix may on the other hand have high resistance to bending and compressive forces, so when used together, produce a composite with both high tensile and compressive strengths and also a high resistance to bending. The matrix binds together the reinforcement, which is usually in the form of rods, strands, fibres or particles and is much stronger and stiffer than the matrix, this results in the reinforcement being held in an orderly pattern and because the reinforcements are usually... [continues]
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(2005, 12). Use of Composites for Aircraft Primary Structural Components. StudyMode.com. Retrieved 12, 2005, from http://www.studymode.com/essays/Use-Composites-Aircraft-Primary-Structural-Components-75786.html
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