AVI-111 Aircraft Materials - Lesson 12: Introduction to Composite Materials

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Vocabulary practice flashcards covering terminology, structural forms, fiber classifications, and properties of advanced composite materials from Lesson 12 of Aircraft Materials (AVI-111).

31 Terms

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Composite Material

A material formed by combining two or more distinct constituents that remain physically identifiable, engineered to produce structural properties superior to those of the individual components.

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Fiber Reinforcement

The primary structural constituent in a composite material that provides most of the tensile strength and stiffness.

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Matrix

The polymer or resin constituent that surrounds and binds reinforcing fibers, transfers applied loads between them, maintains fiber alignment, and provides environmental protection.

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Core Material

A lightweight central structure (such as honeycomb, structural foam, or balsa wood) placed between face sheets to increase bending stiffness and resistance without adding excessive mass.

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Laminated Structure

A composite structural configuration constructed from multiple plies or layers of fiber reinforcement bonded together in selected orientations.

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Sandwich Structure

A structural assembly consisting of two thin, stiff composite face sheets bonded to and separated by a thick, lightweight core material.

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Isotropic Material

A material, such as aluminum or titanium, that exhibits identical mechanical and physical properties in all directions.

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Anisotropic Material

A material, such as a fiber-reinforced composite laminate, whose mechanical properties vary depending on the direction of applied load and fiber orientation.

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Unidirectional Material

A composite reinforcement format where all fibers are parallel in a single direction, offering maximum tensile strength along the fiber axis and virtually no strength across it.

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Bidirectional Material

A woven fabric composite featuring fibers oriented along two perpendicular directions, offering strength across both axes though not necessarily equally.

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Quasi-isotropic Layup

A composite laminate stacking sequence combining plies at multiple angles (such as 0∘0^\circ, 90∘90^\circ, and ±45∘\pm 45^\circ) to simulate isotropic mechanical behavior in all in-plane directions.

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Warp Clock

A directional reference diagram used on engineering drawings to designate the orientation angles of individual composite plies.

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Filament

A single continuous strand of fiber that serves as the basic individual element of a composite reinforcement.

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Tow

An untwisted bundle of continuous filaments gathered together into a strand, also termed a yarn or roving.

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Roving

A bundle of continuous, parallel filaments oriented in the same direction without any twist.

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Prepreg

A ready-to-mold reinforcing fabric or tape pre-impregnated with a thermosetting resin that requires elevated heat and pressure to fully cure.

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Plain Weave

A bidirectional fabric construction where each warp fiber alternates over and under each intersecting fill fiber strand.

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Satin Weave

A fabric weave style where warp bundles float over multiple fill strands before interlacing, yielding high flexibility and drapability over compound curves.

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Nonwoven Fabric

A multi-axial reinforcing material in which straight, parallel fiber plies are stitched together with fine yarns rather than interlaced or woven.

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Whiskers

Tiny, elongated crystalline reinforcing structures that are longer than they are wide, used as discontinuous reinforcement in composite matrices.

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E-glass

An electrical-grade fiberglass formulation that provides high resistance to current flow, commonly used in non-structural aircraft parts and radomes.

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S-glass

A high-tensile-strength structural fiberglass developed specifically for demanding structural applications.

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Kevlar®

A DuPont brand of yellow aramid synthetic fiber known for exceptional tensile strength, lightness, and impact resistance, but prone to moisture absorption and weak in compression.

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Kevlar® 49

A high-stiffness grade of aramid fiber widely utilized in aerospace structural components.

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Kevlar® 29

A lower-stiffness, highly tough grade of aramid fiber commonly used in military ballistic protection and body armor.

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Carbon Fiber

A high-strength, high-stiffness reinforcement with a two-dimensional hexagonal graphene structure, appearing gray or black in color.

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Graphite Fiber

A specialized carbon reinforcement produced through extensive thermal processing to create an ordered three-dimensional crystalline lattice, making it stiffer and more expensive than standard carbon fiber.

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Galvanic Corrosion

An accelerated electrochemical degradation process that occurs when carbon fiber composite laminates are placed in direct electrical contact with metallic fasteners in the presence of moisture.

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Boron Fiber

An exceptionally stiff, high-strength fiber with high tensile and compressive properties, primarily used in military aerospace applications due to high cost and hazardous handling.

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Ceramic Fiber

A high-temperature-resistant reinforcement capable of operating at temperatures up to 2 200 ∘F2\,200\,^\circ\text{F}, such as in gas turbine engine turbine blades.

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Lightning Protection Layer

A conductive outer layer (such as nickel-coated graphite cloth, metal mesh, or conductive paint) applied to composite structures to dissipate high-current lightning strikes.