Aircraft Structure Quiz Reviewer
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Aircraft Structure Quiz Reviewer

Created by
@SweepingXylophone

Questions and Answers

What are the three competing demands that airplane structures need to juggle?

Utmost Safety, Lightweight Durability, Cost-Effectiveness

What does the term 'Fusibility' refer to in material properties?

How easily a material melts when heated

Metal alloys are chosen for aircraft structures due to their exceptional strength in both pulling and pushing forces.

True

_____ is the resistance to scratching or indentation in materials.

<p>Hardness</p> Signup and view all the answers

What are the competing demands that airplane structures must juggle?

<p>Safety, Lightweight Durability, Cost-Effectiveness</p> Signup and view all the answers

Define 'Mechanical Properties' of materials in the context of airplane structure.

<p>Mechanical properties describe how the alloy behaves under force, including strength, ductility, and wear resistance.</p> Signup and view all the answers

Metal alloys are only used in pulling forces in aircraft structures.

<p>False</p> Signup and view all the answers

______ are the workhorses of aircraft structures, chosen for their exceptional strength in both pulling and pushing forces.

<p>Metal alloys</p> Signup and view all the answers

Match the following composites with their common applications:

<p>Glass Fiber Composites = Wind turbine blades, sailplanes, pressure vessels Carbon Fiber Composites = Automotive, aerospace structures Aramid and Kevlar Composites = Bulletproof vests, cockpit doors Fiber Metal Laminates (FMLs) = High strength, fracture toughness</p> Signup and view all the answers

Study Notes

Aircraft Structure Demands

  • Aircraft structures must balance three competing demands: utmost safety, lightweight durability, and cost-effectiveness.

Properties of Materials

Physical Properties

  • Density
  • Melting point
  • Conductivity
  • Thermal expansion

Mechanical Properties

  • Strength: resistance to force
  • Hardness: resistance to scratching or indentation
  • Brittleness: tendency to break without significant bending
  • Toughness: ability to absorb impact
  • Plasticity: permanent deformation under small forces
  • Elasticity: ability to return to original shape after a load is removed
  • Stiffness: resistance to bending under pressure
  • Malleability: ability to be flattened into thin sheets
  • Ductility: ability to be drawn into thin wires
  • Compressive Strength: ability to withstand pushing or squeezing forces
  • Tensile Strength: ability to withstand pulling or stretching forces
  • Durability: resistance to wear, tear, weather, and corrosion

Common Material Used

  • Material Properties: inherent to the material itself (e.g., strength, weight) and independent of its shape
  • Structural Properties: depend on both the material and the design (shape) of the structure
  • Manufacturing Processes: influenced by the material's properties

Interconnected Aspects

  • Changing one aspect can affect the others: material, design, and manufacturing processes

Materials and Their Characteristics

Metal Alloys

  • Exceptional strength in both pulling and pushing forces
  • Examples: Aluminum Alloys, Steel Alloys, Titanium Alloys

Composites

  • Combine multiple materials to create something greater than the sum of its parts
  • Examples: Glass Fiber Composites, Carbon Fiber Composites, Aramid and Kevlar Composites, Fiber Metal Laminates (FMLs)

Aircraft Structure Demands

  • Aircraft structures must balance three competing demands: utmost safety, lightweight durability, and cost-effectiveness.

Properties of Materials

Physical Properties

  • Density
  • Melting point
  • Conductivity
  • Thermal expansion

Mechanical Properties

  • Strength: resistance to force
  • Hardness: resistance to scratching or indentation
  • Brittleness: tendency to break without significant bending
  • Toughness: ability to absorb impact
  • Plasticity: permanent deformation under small forces
  • Elasticity: ability to return to original shape after a load is removed
  • Stiffness: resistance to bending under pressure
  • Malleability: ability to be flattened into thin sheets
  • Ductility: ability to be drawn into thin wires
  • Compressive Strength: ability to withstand pushing or squeezing forces
  • Tensile Strength: ability to withstand pulling or stretching forces
  • Durability: resistance to wear, tear, weather, and corrosion

Common Material Used

  • Material Properties: inherent to the material itself (e.g., strength, weight) and independent of its shape
  • Structural Properties: depend on both the material and the design (shape) of the structure
  • Manufacturing Processes: influenced by the material's properties

Interconnected Aspects

  • Changing one aspect can affect the others: material, design, and manufacturing processes

Materials and Their Characteristics

Metal Alloys

  • Exceptional strength in both pulling and pushing forces
  • Examples: Aluminum Alloys, Steel Alloys, Titanium Alloys

Composites

  • Combine multiple materials to create something greater than the sum of its parts
  • Examples: Glass Fiber Composites, Carbon Fiber Composites, Aramid and Kevlar Composites, Fiber Metal Laminates (FMLs)

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Description

This quiz reviews the competing demands of aircraft structures, including safety, lightweight durability, and cost-effectiveness, as well as the physical and mechanical properties of materials used in their construction.

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