Engineering Chemistry

Chapter 9
Metals, Alloys, Ceramics and Composite Materials

Bachelor Program in Mechatronics Engineering
Engineering Chemistry   •   Bachelor

Metals, Alloys, Ceramics and Composite Materials

Introduction and Context

Materials determine what a mechatronic system can sense, support, transmit, insulate, dissipate, or survive. A robotic arm, for example, may combine an aluminium alloy frame, hardened steel gears, ceramic electrical insulation, polymer-matrix composite covers, copper conductors, and bonded or bolted joints. Selecting these materials requires more than comparing strength or price. Performance emerges from the relationship between composition, atomic bonding, crystal structure, defects, processing history, environment, and service conditions.

This chapter develops a structure–processing–properties–performance framework for metals, alloys, ceramics, and composite materials. It emphasizes how engineering chemistry supports materials selection and manufacturing decisions in mechatronics.

Learning Objectives

By the end of this chapter, students should be able to:

  1. Relate metallic, ionic, covalent, and van der Waals bonding to material properties.
  2. Describe common crystal structures and explain the engineering importance of defects.
  3. Distinguish pure metals, solid solutions, intermetallic compounds, ceramics, and composites.
  4. Interpret basic binary phase diagrams and explain phase transformations.
  5. Explain how deformation, heat treatment, sintering, casting, forming, machining, and composite processing affect properties.
  6. Compare materials using mechanical, thermal, electrical, chemical, and manufacturing criteria.
  7. Apply material-selection reasoning to a mechatronic component.
  8. Recognize limitations, sustainability issues, and safety responsibilities associated with engineering materials.

1. Composition, Bonding, and Material Behaviour

1.1 Chemical composition as a design variable

A material’s composition specifies the elements and their relative amounts. Small additions can produce large changes. Carbon contents below about 1 mass percent can substantially alter the hardness and heat-treatment response of iron. Chromium promotes corrosion resistance in stainless steels, while silicon improves the castability of aluminium alloys. In ceramics, controlled additions of yttria can stabilize zirconia and improve toughness.

Composition is not the same as microstructure. Two components with the same nominal composition may have different grain sizes, phases, porosity, and residual stresses because they were processed differently. Consequently, a material specification should identify not only chemistry but also condition—for example, an aluminium alloy in a specified precipitation-hardened temper.

1.2 Primary chemical bonds

Metallic bonding results when valence electrons are relatively delocalized among many atoms. Metallic bonds are non-directional, allowing atomic planes to slip when sufficient stress is applied. This helps explain ductility, toughness, electrical conductivity, and thermal conductivity. The same mobile electrons also allow metals to reflect light and respond strongly to electromagnetic fields.

Ionic bonding involves electron transfer and electrostatic attraction between oppositely charged ions. Sodium chloride is a simple example. Ionic solids generally have high melting temperatures, high stiffness, and low room-temperature ductility because moving one plane can bring like charges into close proximity, producing strong repulsion and fracture.

Covalent bonding involves shared electrons between particular atoms. Bonds are directional, as in silicon, silicon carbide, and diamond. Directionality produces high stiffness and hardness but often restricts plastic deformation. Network covalent solids can therefore be strong yet brittle.

Secondary bonding, including hydrogen bonding and van der Waals attraction, is weaker than primary bonding but important in polymers, layered solids, coatings, and interfaces. Composite performance is often governed by secondary bonding or chemical coupling at the matrix–reinforcement interface.

No engineering material is perfectly represented by one bond type. Ceramics often contain mixed ionic–covalent bonding, and metallic alloys may contain phases with different bonding character.

2. Crystal Structures and Defects

2.1 Crystalline and amorphous structures

A crystalline solid has long-range atomic order. An amorphous solid has no repeating long-range lattice, although it may possess short-range order. Most engineering metals are crystalline; ordinary glass is amorphous; many polymers are partly crystalline and partly amorphous.

The repeating unit of a crystal is described by a unit cell. Important metallic structures include:

StructureTypical featureExamplesEngineering significance
Body-centred cubic (BCC)Atom at each corner and one at the centreα-iron, chromium, tungstenOften strong; slip is more temperature-sensitive
Face-centred cubic (FCC)Atoms at corners and face centresAluminium, copper, nickel, γ-ironMany slip systems; usually ductile
Hexagonal close-packed (HCP)Hexagonal stackingMagnesium, titanium, zincFewer easy slip systems; directional plasticity

The coordination number is the number of nearest neighbours around an atom. The atomic packing factor is the fraction of unit-cell volume occupied by idealized atoms:

APF = (volume occupied by atoms in a unit cell) ÷ (unit-cell volume)

For ideal hard-sphere models, FCC and HCP have APF ≈ 0.74, BCC has APF ≈ 0.68, and simple cubic has APF ≈ 0.52. These values are geometric models, not direct measures of strength or density.

2.2 Crystal defects

Real crystals contain defects, and controlled defects are essential to engineering design.

Point defects include vacancies, interstitial atoms, and substitutional atoms. Vacancy concentration increases with temperature and can be represented approximately by:

Nv/N = exp(−Qv/(R T))

where Nv is the number of vacancies, N is the number of atomic sites, Qv is vacancy formation energy in J mol⁻¹, R is the gas constant, and T is absolute temperature in kelvin. This expression assumes thermodynamic equilibrium and neglects interactions among defects.

Dislocations are line defects. An edge dislocation contains an extra half-plane of atoms; a screw dislocation produces a helical lattice distortion. Plastic deformation in crystalline metals occurs mainly through dislocation motion. Strengthening methods impede this motion:

  • grain refinement;
  • solid-solution strengthening;
  • precipitation or dispersion strengthening;
  • work hardening; and
  • transformation hardening.

The Hall–Petch relationship describes the influence of average grain diameter on yield strength:

σy = σ0 + ky d^(−1/2)

where σy is yield stress, σ0 is the friction stress, ky is the Hall–Petch coefficient, and d is average grain diameter. Units must be consistent: if d is in metres, ky must have units of Pa·m^(1/2). The relationship is an empirical approximation over a suitable grain-size range; extremely fine grains can show departures from it.

Planar defects include grain boundaries, phase boundaries, stacking faults, and twin boundaries. Grain boundaries can block dislocations and increase strength, but they may also act as paths for diffusion, corrosion, or creep damage.

Volume defects include pores, inclusions, voids, cracks, and segregated regions. Even a small crack can greatly reduce tensile strength because it concentrates stress. In brittle ceramics and composites, flaw control is often more important than nominal theoretical strength.

3. Metals and Alloys

3.1 Pure metals and alloys

A pure metal contains one principal element, whereas an alloy contains a metal combined with one or more elements. Alloys are designed to modify strength, corrosion resistance, conductivity, density, melting range, machinability, or magnetic behaviour.

A solid solution forms when solute atoms occupy positions in a solvent lattice. In a substitutional solid solution, solute and solvent atoms replace one another; in an interstitial solid solution, small atoms occupy spaces between host atoms. Solubility depends on atomic size, crystal structure, valence, and chemical affinity.

An intermetallic compound has a relatively ordered composition and structure, such as Ni₃Al. Intermetallics can provide high-temperature strength but may be brittle at room temperature. A second phase may be intentionally formed as particles within a matrix, producing precipitation hardening.

3.2 Mechanical behaviour

The engineering normal stress is:

σ = F/A0

where F is axial force in newtons and A0 is original cross-sectional area in square metres. Engineering strain is:

ε = (L − L0)/L0 = ΔL/L0

where L0 and L are the original and current gauge lengths. These definitions are most useful for small to moderate deformation; true stress and true strain are preferable for large plastic deformation.

In the linear elastic region, Hooke’s law is:

σ = E ε

where E is Young’s modulus in pascals. This relation applies only while the material behaves linearly and elastically. On unloading within the elastic range, the specimen returns to its original dimensions.

Strength is resistance to yielding or fracture. Hardness is resistance to indentation or scratching. Toughness is the energy absorbed before fracture, represented by the area under a stress–strain curve. Ductility describes plastic strain before fracture. These properties are not interchangeable: a very hard ceramic may have low fracture toughness, while a softer metal may be highly damage tolerant.

3.3 Strengthening and heat treatment

Cold working increases dislocation density and raises strength and hardness, but reduces ductility. Recovery reduces some residual stress; recrystallization forms new strain-free grains; grain growth may reduce strength.

In steels, heating and cooling can produce ferrite, pearlite, bainite, or martensite. Rapid quenching can form hard martensite, but it may also cause distortion and cracking. Tempering reduces brittleness while retaining useful strength. In aluminium, copper, nickel, and some titanium alloys, solution treatment, quenching, and ageing produce fine precipitates that obstruct dislocations.

Heat treatment must be specified with temperature, time, atmosphere, heating and cooling rates, and component dimensions. A nominal recipe may fail if the centre of a thick part does not experience the intended thermal cycle.

3.4 Thermal, electrical, and chemical behaviour

Electrical resistivity generally increases with temperature in pure metals because lattice vibrations scatter electrons. Alloying increases electron scattering and therefore often increases resistivity. Copper and aluminium are widely used as conductors; nickel alloys are used where resistance and high-temperature stability are desired.

The linear thermal expansion approximation is:

ΔL = α L0 ΔT

where α is the coefficient of linear thermal expansion in K⁻¹, L0 is original length, and ΔT is temperature change in kelvin or degrees Celsius. It assumes approximately constant α over the temperature interval and unconstrained expansion.

Metals may corrode by electrochemical reactions. Corrosion prevention includes alloying, coatings, passivation, cathodic protection, drainage, isolation of dissimilar metals, and environmental control. Galvanic corrosion occurs when dissimilar conductive materials are electrically connected in an electrolyte; its severity depends on potential difference, area ratio, electrolyte chemistry, and oxygen availability.

4. Ceramics and Glasses

Ceramics are inorganic, non-metallic materials produced from compounds such as oxides, carbides, nitrides, silicates, and borides. Traditional ceramics include bricks and porcelain; advanced ceramics include alumina, zirconia, silicon carbide, silicon nitride, and piezoelectric lead-free compositions.

Ceramics usually exhibit high hardness, compressive strength, melting or decomposition temperature, corrosion resistance, and electrical insulation. Their limitations include low tensile ductility, sensitivity to flaws, difficult machining, and thermal-shock vulnerability.

A ceramic’s tensile failure is often governed by the largest critical flaw. Linear elastic fracture mechanics gives the stress-intensity relation:

KI = Y σ √(π a)

where KI is mode-I stress intensity in MPa√m, Y is a dimensionless geometry factor, σ is applied tensile stress, and a is crack or flaw size in metres. Fracture occurs when KI reaches the material’s fracture toughness KIC, subject to appropriate geometry, loading, and small-scale yielding assumptions. Ceramics have little plastic relaxation, so reducing flaw size and tensile stress is crucial.

Ceramic powder processing commonly includes powder preparation, mixing, shaping, drying, debinding, and sintering. During sintering, diffusion reduces pore volume and bonds particles. Excessive grain growth or residual porosity can reduce strength. Hot pressing and hot isostatic pressing can produce higher density but increase equipment and cost.

Glasses are generally amorphous. Their properties can be modified by composition and thermal treatment. Tempered glass contains beneficial surface compressive stress, improving resistance to surface cracks. Glass ceramics use controlled crystallization to combine selected glass-processing advantages with improved thermal or mechanical properties.

5. Composite Materials

A composite combines two or more distinct phases to obtain a property balance not readily achieved by one material. The continuous matrix binds and protects the reinforcement, transfers load, and often determines environmental resistance. Reinforcements may be particles, short fibres, continuous fibres, whiskers, flakes, or structural cores.

Examples include:

  • glass-fibre-reinforced polymer (GFRP);
  • carbon-fibre-reinforced polymer (CFRP);
  • aluminium reinforced with silicon carbide particles;
  • concrete, with cement paste and aggregate; and
  • sandwich panels with strong skins and a lightweight core.

The longitudinal elastic modulus of a continuous unidirectional fibre composite can be estimated by the rule of mixtures:

EL = Vf Ef + Vm Em

where EL is longitudinal modulus, Vf and Vm are fibre and matrix volume fractions, and Ef and Em are their moduli. The equation assumes aligned, continuous fibres, effective load transfer, uniform distribution, and elastic loading. Since Vf + Vm = 1, the expression is a weighted average.

For transverse loading, a simple inverse estimate is:

1/ET = Vf/Ef + Vm/Em

This relation is an idealized lower-bound-type model and is not universally accurate, particularly for imperfect interfaces, voids, woven architectures, or nonlinear matrices.

Composite anisotropy is both an advantage and a hazard. Fibres can be placed along principal load paths, but properties across the fibre direction may be much lower. Failure modes include fibre fracture, matrix cracking, interface debonding, delamination, buckling, and environmental degradation.

Manufacturing methods include hand lay-up, resin transfer moulding, filament winding, pultrusion, compression moulding, prepreg autoclave processing, metal-matrix casting, and additive manufacturing. Key process variables include fibre volume fraction, cure temperature, pressure, moisture, void content, and fibre alignment.

6. Phase Diagrams and Phase Transformations

A phase is a chemically and physically uniform region with a defined structure and composition range. A phase diagram maps stable or equilibrium phases as functions of variables such as temperature, pressure, and composition.

A binary temperature–composition diagram may contain liquid, solid, or two-phase regions. In a two-phase region, the compositions of the phases are found using a horizontal tie line. The lever rule estimates phase fractions. For an overall composition C0, with phase compositions C_α and C_β, the fraction of α is:

f_α = (C_β − C0)/(C_β − C_α)

and the fraction of β is:

f_β = (C0 − C_α)/(C_β − C_α)

All compositions must use the same basis, such as mass percent or mole fraction. The fractions should sum to one. The lever rule applies to an equilibrium two-phase region and does not by itself predict phase morphology or transformation rate.

Important reactions include eutectic transformation, in which one liquid forms two solid phases, and eutectoid transformation, in which one solid phase forms two different solid phases. Phase diagrams are equilibrium maps; real processing may produce metastable phases because diffusion is limited. Time–temperature–transformation and continuous-cooling-transformation diagrams are therefore needed when transformation kinetics matter.

7. Processing and Manufacturing Relationships

Casting shapes liquid material in a mould. It is economical for complex geometries but may produce porosity, segregation, shrinkage, and coarse grains. Solidification rate and thermal gradients strongly influence microstructure.

Forming processes such as rolling, forging, extrusion, and drawing plastically deform solid material. They can improve strength through work hardening and produce directional grain flow. Excessive deformation without intermediate annealing can cause cracking.

Machining removes material and offers dimensional accuracy, but cutting generates heat and may leave residual stress or surface damage. Tool choice depends on hardness, thermal conductivity, chemical reactivity, and abrasive particles.

Powder metallurgy mixes, compacts, and sinters powders. It can reduce waste and produce near-net shapes, but powder contamination, density gradients, and residual porosity require control.

Additive manufacturing builds components layer by layer. It enables internal channels, lattice structures, and rapid iteration, but anisotropy, surface roughness, porosity, residual stress, and qualification remain important concerns.

Joining methods include welding, brazing, soldering, adhesive bonding, mechanical fastening, and diffusion bonding. The joint may be the weakest part of an assembly. Thermal expansion mismatch, galvanic coupling, adhesive ageing, and inspection access must be considered during design.

8. Engineering Selection Framework

A defensible selection process begins with function rather than a preferred material. The engineer should:

  1. define loads, motion, temperature, environment, electrical requirements, life, and safety factors;
  2. identify constraints such as mass, envelope, cost, supply, and manufacturing capability;
  3. screen materials using required properties;
  4. consider processing, joining, inspection, repair, and recycling;
  5. assess failure modes and uncertainty;
  6. prototype and test under representative conditions; and
  7. document the selection and verification evidence.

Useful performance indices include specific stiffness and specific strength:

specific stiffness = E/ρ
specific strength = σy/ρ

where E is modulus, σy is yield strength, and ρ is density. These indices are useful when low mass is important, but they do not replace consideration of fatigue, fracture, joints, cost, fire behaviour, corrosion, or manufacturability.

RequirementOften favourable choicesImportant cautions
Low mass and moderate stiffnessAluminium alloys, magnesium alloys, CFRPCorrosion, anisotropy, joining, cost
High wear resistanceHardened steel, ceramics, cermetsBrittleness, machining difficulty
Electrical conductionCopper, aluminium, selected metal alloysMass, oxidation, thermal expansion
Electrical insulationAlumina, glass, polymersDielectric breakdown, thermal shock
High-temperature structureNickel alloys, ceramics, SiC compositesOxidation, creep, brittle failure
Vibration reductionPolymers, elastomers, sandwich compositesAgeing, temperature dependence

9. Illustrative Case Study: Material Selection for a Robotic Joint Housing

Background

A university–industry team is designing a compact robotic joint for a collaborative manipulator. The housing supports a gearbox, carries moderate bending loads, contains a motor and sensors, and must dissipate heat while remaining light enough for the robot arm.

Problem

The initial steel housing is strong but heavy. The housing must resist fatigue, maintain dimensional accuracy, tolerate workshop humidity, provide electromagnetic shielding, and be manufacturable in small production batches. The design team compares ductile iron, aluminium alloy, magnesium alloy, and a carbon-fibre composite shell with metallic inserts.

Analysis

Ductile iron offers stiffness, damping, and good castability but increases arm mass. Aluminium provides low density, good machinability, and thermal conductivity, but its modulus is lower than steel and threaded regions may require inserts. Magnesium is lighter but demands stronger corrosion and fire controls. CFRP offers high specific stiffness and corrosion resistance, but the joint contains concentrated bearing loads and threaded attachments that complicate load transfer and inspection.

The team identifies the dominant failure modes as housing deflection, bearing-seat distortion, fatigue cracking, galvanic corrosion, and thermal misalignment. They use finite-element analysis for stress and deflection, but treat simulation as a model requiring experimental validation. Prototype housings are tested under combined torque, radial load, thermal cycling, and vibration.

Approach and solution

An aluminium alloy housing is selected with local steel or stainless-steel inserts at bearing seats and high-load threads. The design uses generous radii to reduce stress concentration, a hard anodized surface for wear and corrosion protection, sealed interfaces, and controlled electrical isolation from carbon-steel fasteners. The motor mounting region includes fins to improve heat transfer. A gasket and drainage path prevent trapped moisture.

The material decision is not based solely on the highest strength. It balances density, stiffness, thermal conductivity, machining, corrosion, joining, inspection, and total lifecycle cost.

Outcome

Testing confirms acceptable deflection and temperature rise. The aluminium design reduces mass substantially relative to the cast-iron baseline while preserving bearing alignment. The project also discovers that the adhesive sealant selected initially loses stiffness at the upper operating temperature, so it is replaced with a qualified sealant and mechanical retention.

Learning points

  1. Material selection is inseparable from joint and manufacturing design.
  2. Local inserts can solve concentrated-load problems but introduce interfaces and galvanic risks.
  3. Thermal expansion and sealing require explicit analysis.
  4. Simulation must be supported by representative testing.
  5. The lightest candidate is not automatically the best engineering solution.

10. Limitations, Sustainability, and Professional Responsibility

Material data are commonly reported as ranges because properties vary with composition, processing, temperature, orientation, moisture, defects, and test method. Design values should include appropriate reliability and safety considerations rather than using attractive catalogue maxima.

Sustainability requires life-cycle thinking. Aluminium production is energy intensive but recycling can be advantageous. Steel has established recycling infrastructure. Composite recycling is more difficult because fibres and matrices are bonded, although thermoplastic matrices, mechanical reclamation, pyrolysis, solvolysis, and design for disassembly are developing. Ceramic production may require high-temperature furnaces, while mining and refining can create ecological and social impacts.

Engineers must consider worker exposure to metal dust, ceramic fibres, solvents, resins, fumes, and nanoparticles. Safety data sheets, ventilation, personal protective equipment, waste controls, and applicable standards are essential. Material substitutions must not compromise fire safety, electrical isolation, structural integrity, or environmental compliance.

Digital tools and artificial intelligence can help search databases, optimize composition, predict defects, and explore process windows. However, AI-generated recommendations may contain inaccurate data, hidden assumptions, or extrapolation beyond validated conditions. Engineers remain responsible for traceable sources, testing, confidentiality, and final decisions.

Chapter Summary

Material performance results from the interaction of composition, bonding, crystal structure, defects, phases, processing, and service environment. Metallic bonding supports conductivity and ductility, whereas ionic and covalent bonding commonly produce hard, temperature-resistant but brittle ceramics. Crystal defects are not merely imperfections: dislocations enable plasticity, vacancies enable diffusion, and grain boundaries influence strength, corrosion, and transformation.

Alloys modify pure-metal behaviour through solid solution, second phases, precipitation, and heat treatment. Ceramics provide hardness, insulation, corrosion resistance, and high-temperature capability but are sensitive to flaws and tensile fracture. Composites combine matrix and reinforcement to provide tailored stiffness, strength, density, and anisotropy. Phase diagrams identify equilibrium phase fields and provide tools such as the tie line and lever rule, although kinetics and processing history determine actual microstructures.

Sound mechatronic material selection integrates mechanical, thermal, electrical, chemical, manufacturing, joining, lifecycle, safety, and cost requirements. Prototypes and tests are necessary because real components contain defects, interfaces, residual stresses, and environmental exposures not fully represented by simple equations or simulations.

Key Terms

Bonding: Atomic interaction that holds a solid together.

Alloy: Metallic material containing a principal metal and one or more additional elements.

Crystal lattice: Repeating three-dimensional arrangement of atoms or ions.

Unit cell: Smallest repeating geometric description of a crystal structure.

Dislocation: Line defect that enables plastic deformation in crystals.

Vacancy: Missing atom from an otherwise occupied lattice site.

Grain boundary: Interface between crystals of different orientations.

Solid solution: Single phase containing solute atoms within a solvent lattice.

Intermetallic compound: Ordered compound formed between metallic elements.

Phase: Chemically and physically uniform region of a material.

Phase diagram: Map of equilibrium phases as functions of composition and other variables.

Heat treatment: Controlled thermal cycle used to modify microstructure and properties.

Ceramic: Inorganic, non-metallic material commonly containing ionic or covalent compounds.

Toughness: Capacity to absorb energy before fracture.

Fracture toughness: Resistance to crack extension under defined loading conditions.

Composite: Material made from distinct matrix and reinforcement phases.

Matrix: Continuous phase that binds and supports composite reinforcement.

Anisotropy: Dependence of properties on direction.

Sintering: Thermal bonding and densification of a compacted powder.

Galvanic corrosion: Electrochemical corrosion caused by contact between dissimilar conductive materials in an electrolyte.

Review Questions

Short Answer Questions

  1. How does metallic bonding contribute to the ductility and electrical conductivity of metals?
  2. Distinguish a vacancy, dislocation, and grain boundary.
  3. Why are ceramics generally strong in compression but vulnerable in tension?
  4. What functions are performed by the matrix in a fibre-reinforced composite?
  5. Why is a phase diagram insufficient for predicting every real processing result?

Long Answer Questions

  1. Explain how composition, crystal structure, defects, and heat treatment can be combined to strengthen an alloy.
  2. Compare metals, ceramics, and composites for a high-temperature, electrically insulating mechatronic component.
  3. Describe the complete powder-processing route for a ceramic part and identify possible defect sources.
  4. Explain the rule of mixtures for a unidirectional composite, including its assumptions and limitations.
  5. Develop a material-selection procedure for a lightweight robotic arm link exposed to cyclic loading and humidity.

Analytical / Application Questions

  1. A two-phase alloy has overall composition C0 = 40 mass% solute. At the processing temperature, phase α contains C_α = 20 mass% solute and phase β contains C_β = 70 mass% solute. Use the lever rule to calculate the mass fraction of each phase and verify that the fractions sum to one.
  2. A component is made from a unidirectional composite with fibre volume fraction 0.60, fibre modulus 70 GPa, and matrix modulus 3 GPa. Estimate its longitudinal modulus using the rule of mixtures. State why the estimate may differ from a tested value.
  3. A designer proposes replacing a steel gearbox housing with a carbon-fibre composite solely because the composite has a higher specific stiffness. Critically evaluate the proposal, considering bearing seats, threads, impact, thermal expansion, electromagnetic shielding, joining, inspection, repair, and lifecycle issues.

Multiple Choice Questions with Answers

Question 1

Which crystal structure generally provides many easily activated slip systems and high room-temperature ductility?

A. Face-centred cubic

B. Body-centred cubic

C. Hexagonal close-packed

D. Amorphous glass

Correct Answer: A. Face-centred cubic

Question 2

In the Hall–Petch relationship, decreasing grain size usually causes yield strength to:

A. Decrease because grain boundaries disappear

B. Increase because grain boundaries impede dislocation motion

C. Remain unchanged for all materials

D. Become equal to Young’s modulus

Correct Answer: B. Increase because grain boundaries impede dislocation motion

Question 3

Which defect is primarily responsible for enabling plastic deformation in crystalline metals?

A. Pore

B. Vacancy cluster

C. Dislocation

D. Inclusion

Correct Answer: C. Dislocation

Question 4

A ceramic component is most likely to fail when tensile stress intensity reaches its:

A. Thermal conductivity

B. Fracture toughness

C. Atomic packing factor

D. Electrical resistivity

Correct Answer: B. Fracture toughness

Question 5

For a two-phase alloy, the lever rule is used primarily to estimate:

A. The density of a single atom

B. The phase fractions in an equilibrium two-phase region

C. The machining power required

D. The crack-tip temperature

Correct Answer: B. The phase fractions in an equilibrium two-phase region

Question 6

Which processing operation commonly increases the strength and hardness of a metal while reducing ductility?

A. Cold working

B. Complete annealing only

C. Stress-free casting

D. Glass tempering

Correct Answer: A. Cold working

Question 7

A composite matrix primarily:

A. Eliminates all anisotropy

B. Binds reinforcement and transfers load

C. Acts only as a decorative coating

D. Prevents every possible failure mode

Correct Answer: B. Binds reinforcement and transfers load

Question 8

If a composite has fibre volume fraction 0.5, fibre modulus 100 GPa, and matrix modulus 4 GPa, the longitudinal rule-of-mixtures modulus is:

A. 4 GPa

B. 48 GPa

C. 52 GPa

D. 104 GPa

Correct Answer: C. 52 GPa

Question 9

Which material is generally most suitable for electrical conduction in ordinary wiring?

A. Alumina

B. Silicon carbide

C. Copper

D. Porcelain

Correct Answer: C. Copper

Question 10

Galvanic corrosion requires, among other conditions:

A. Two dissimilar conductive materials electrically connected in an electrolyte

B. Only a dry inert gas and one pure ceramic

C. A vacuum and identical metals

D. A material with no electrochemical potential

Correct Answer: A. Two dissimilar conductive materials electrically connected in an electrolyte

Engineering Chemistry
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