Electro Magnetic Field

Chapter 14
Multiphysics and Contemporary Engineering Applications

Post Graduate Program in Electrical Engineering
Electro Magnetic Field   •   Post Graduate

Multiphysics and Contemporary Engineering Applications

Introduction

Modern electromagnetic devices rarely operate as purely electromagnetic systems. Electric currents generate heat; fields exert forces; temperature changes conductivity, permeability, and dimensions; fluid motion transports heat and may induce currents; deformation changes air gaps and resonant frequencies. Multiphysics analysis treats these interactions as a coupled system rather than as unrelated corrections.

Applications include electrical machines, transformers, induction furnaces, magnetic bearings, plasma devices, wireless-power systems, MRI magnets, electromagnetic launchers, high-frequency electronics, electric-vehicle powertrains, and magnetohydrodynamic systems. Reliable analysis requires physically consistent governing equations, interface conditions, timescale assessment, numerical coupling, and experimental validation.

Learning Objectives

After completing this chapter, the reader should be able to:

  • formulate electromagnetic–thermal–fluid–mechanical models;
  • identify one-way and two-way coupling mechanisms;
  • calculate electromagnetic losses, skin depth, force, and thermal response;
  • include advective heat transport in moving fluids;
  • apply Maxwell stress with the required momentum-storage qualification;
  • select sequential, iterative, or monolithic numerical coupling;
  • evaluate uncertainty, stability, validation, and safety in contemporary applications.

1. Multiphysics Coupling Architecture

A multiphysics model consists of field equations connected through shared source terms, material properties, geometry, and boundary conditions.

Electromagnetic, thermal, fluid and mechanical coupling Electromagnetic E, H, J, B Thermal T, heat flux Mechanical displacement, stress Fluid velocity, pressure Joule, dielectric and core losses temperature-dependent properties force and torque geometry advection/convection buoyancy and properties pressure and shear deformation and contact
Correct coupling relationships among electromagnetic, thermal, fluid and mechanical fields
Figure: Correct coupling relationships among electromagnetic, thermal, fluid and mechanical fields

Figure: Physically consistent interactions among electromagnetic, thermal, fluid, and mechanical fields. Fluid flow transports heat by advection and convection.

1.1 Coupling classifications

  • One-way coupling: one field affects another without significant feedback. For example, calculated winding losses may be transferred to a thermal model with fixed electrical properties.
  • Two-way coupling: feedback is important. Copper heating increases resistance, which changes current distribution and loss.
  • Weak coupling: exchanged quantities cause relatively small changes and can often be solved sequentially.
  • Strong coupling: feedback materially affects stability or accuracy and requires iteration or a monolithic solution.
  • Multirate coupling: subsystems have different characteristic times. Electromagnetic periods may be microseconds, while thermal transients last minutes.

2. Electromagnetic Formulation

2.1 Maxwell equations

The macroscopic differential equations are

∇ × E = −∂B/∂t, ∇ × H = J + ∂D/∂t
∇ · B = 0, ∇ · D = ρe

Here, E is electric field intensity (V·m⁻¹), H is magnetic field intensity (A·m⁻¹), D is electric flux density (C·m⁻²), B is magnetic flux density (T), J is conduction current density (A·m⁻²), and ρe is free-charge density (C·m⁻³).

For linear isotropic media, D = εE, B = μH, and J = σE, where ε, μ, and σ denote permittivity, permeability, and conductivity. Nonlinear, anisotropic, dispersive, and hysteretic materials require more general constitutive laws.

2.2 Eddy-current approximation

When displacement current is negligible compared with conduction current, Ampère's law becomes ∇ × H ≈ J. Introducing magnetic vector potential B = ∇ × A and electric potential φ,

E = −∂A/∂t − ∇φ

The conducting-region equation is

∇ × (μ−1∇ × A) + σ(∂A/∂t + ∇φ) = Js

where Js is an impressed source-current density. Charge continuity supplies

∇ · [σ(∂A/∂t + ∇φ)] = 0

These equations assume that capacitive effects are unimportant. They are unsuitable where wave propagation, radiation, or significant dielectric displacement current occurs.

2.3 Electromagnetic power deposition

Instantaneous conduction heating is

qJ = J · E

where qJ has units W·m⁻³. For sinusoidal steady state represented by peak phasors,

q̄J = ½ Re{J · E*}

The asterisk denotes complex conjugation. If RMS phasors are used, the factor ½ is omitted.

For a linear lossy dielectric using peak phasors and the ejωt convention,

q̄d = ½ωε''|E|²

where ε'' > 0 is the dielectric-loss component. Magnetic-core loss is commonly obtained from measured loss maps or a calibrated hysteresis model; a universal power law should not be assumed outside its measured frequency and flux-density range.

2.4 Skin depth

For a good, homogeneous conductor with σ ≫ ωε and approximately constant permeability,

δ = √(2/(ωμσ))

Here δ is skin depth (m) and ω = 2πf is angular frequency (rad·s⁻¹). The formula describes exponential penetration into a locally planar semi-infinite conductor.

Worked Example 1: Copper skin depth

For copper at 100 kHz, take σ = 5.8 × 107 S·m−1 and μ = μ0 = 1.2566 × 10−6 H·m−1. Then

δ = √[2/(2π × 105 × 1.2566 × 10−6 × 5.8 × 107)]
= 2.09 × 10−4 m ≈ 0.209 mm

Thus, conductors several millimetres thick exhibit substantial current crowding at this frequency.

3. Electromagnetic Force and Mechanical Response

3.1 Force density

In vacuum or for explicitly resolved free charges and currents, the Lorentz force density is

f = ρeE + J × B

The expression has units N·m⁻³. In magnetizable or polarizable matter, macroscopic force-density formulations require care because different stress descriptions partition field and material momentum differently. A robust engineering method is to integrate stress over a surface lying in vacuum or air outside the body.

3.2 Maxwell stress and momentum storage

For a closed surface S in vacuum enclosing material volume V, the total electromagnetic force on the enclosed matter is

F = ∮S TEM · n dS − d/dt ∫V gEM dV

where n is the outward unit normal, gEM = ε0E × B is vacuum electromagnetic momentum density (N·s·m⁻³), and

TEM = ε0(EE − ½|E|²I) + μ0−1(BB − ½|B|²I)

Here EE and BB are dyadic products and I is the identity tensor. The commonly used surface integral alone is valid in static or quasistatic conditions when momentum storage is negligible, or as a cycle average in periodic steady state because the average time derivative over a complete period is zero. It must not be presented as an unrestricted transient-force law.

3.3 Structural equation

For a deformable solid,

ρs ∂²d/∂t² = ∇ · σm + fEM + ρsg

where d is displacement (m), ρs is solid density (kg·m⁻³), σm is mechanical Cauchy stress (Pa), and fEM is electromagnetic body force (N·m⁻³). For linear thermoelasticity,

ε = ½(∇d + ∇dT), σm = C:[ε − αT(T−T0)I]

where C is the elasticity tensor and αT is the coefficient of thermal expansion (K⁻¹).

Electromagnetic deformation can alter air gaps, inductance, force harmonics, and acoustic noise. This feedback is critical in magnetic bearings, relays, transformers, and high-torque machines.

4. Thermal and Moving-Fluid Formulation

4.1 General internal-energy balance

For a moving continuum,

ρ De/Dt = −∇ · q − p∇ · u + τ:∇u + qEM + qother

Here e is specific internal energy (J·kg⁻¹), D/Dt = ∂/∂t + u·∇ is the material derivative, q is conductive heat flux (W·m⁻²), p is pressure (Pa), u is fluid velocity (m·s⁻¹), and τ is viscous stress (Pa). Fourier conduction gives q = −k∇T.

For an incompressible, constant-property fluid with negligible pressure work, the temperature equation becomes

ρcp(∂T/∂t + u · ∇T) = ∇ · (k∇T) + qEM + Φ + qother

where cp is specific heat capacity (J·kg⁻¹·K⁻¹), k is thermal conductivity (W·m⁻¹·K⁻¹), and Φ = τ:∇u is viscous dissipation (W·m⁻³). The term ρcpu·∇T represents advective heat transport and must be included when the coolant moves. In a stationary solid, u = 0, reducing the equation to transient heat conduction.

Phase change is more conveniently represented using enthalpy so that latent heat is included without imposing an artificial temperature jump.

4.2 Fluid momentum and mass conservation

For an incompressible Newtonian fluid,

∇ · u = 0
ρ(∂u/∂t + u · ∇u) = −∇p + μf∇²u + ρg + fEM

where μf is dynamic viscosity (Pa·s). In conducting fluids, fEM may include J × B. Temperature can affect the flow through density-dependent buoyancy, viscosity, and conductivity.

Worked Example 2: Advective heating of a coolant

A liquid with ρ = 997 kg·m−3 and cp = 4180 J·kg−1·K−1 moves at uniform velocity u = 0.20 m·s−1 through a 0.50 m region. It experiences uniform volumetric electromagnetic heating qEM = 2.0 × 106 W·m−3. Neglect axial conduction, wall heat transfer, and property variation.

For steady one-dimensional plug flow,

ρcpu dT/dx = qEM

Therefore,

∆T = qEML/(ρcpu)
= (2.0 × 106 × 0.50)/(997 × 4180 × 0.20)
≈ 1.20 K

This calculation explicitly accounts for heat carried downstream by fluid motion.

4.3 Dimensionless indicators

The thermal Péclet number compares advection with conduction:

Pe = ρcpUL/k = UL/α

where L is characteristic length, U is characteristic velocity, and α = k/(ρcp) is thermal diffusivity. Large Pe indicates dominant advective transport.

For a moving conductor, the magnetic Reynolds number is

Rm = μσUL

When Rm ≪ 1, magnetic fields induced by bulk fluid motion are often small relative to the imposed field. This does not imply that the Lorentz force is negligible.

5. Interface and Boundary Conditions

Correct interface conditions are as important as the differential equations.

Electromagnetic interfaces

In the absence of imposed surface electric current and magnetic surface charge,

n × (E2 − E1) = 0, n · (B2 − B1) = 0

If a surface current density Ks exists,

n × (H2 − H1) = Ks

The normal electric-flux jump equals free surface-charge density.

Thermal interfaces

For ideal thermal contact without interfacial generation,

T1 = T2, n · k1∇T1 = n · k2∇T2

A contact resistance R''th gives

q'' = (T1 − T2)/R''th

Convective heat transfer at a wall is often represented by

−n · k∇T = h(Ts − T_∞)

where h is a heat-transfer coefficient (W·m⁻²·K⁻¹). When computational fluid dynamics resolves the coolant, heat transfer should instead arise from continuity of temperature and normal heat flux at the fluid–solid interface; imposing an additional empirical h there would double-count convection.

Fluid and mechanical interfaces

A stationary impermeable wall commonly uses no slip, u = 0. A moving wall uses continuity between wall and fluid velocity. Fluid–structure interaction additionally enforces traction equilibrium and compatible motion at the interface.

6. Feedback, Nonlinearity, and Stability

Material properties may depend strongly on temperature and field:

σ = σ(T), μ = μ(H,T), ε = ε(E,T,ω), k = k(T)

For a metallic conductor near a reference temperature,

R(T) = R0[1 + αR(T−T0)]

This linear approximation is valid only over the range for which αR is representative.

Worked Example 3: Electrothermal feedback

A current-driven coil has I = 100 A, R0 = 0.020 Ω, αR = 0.0039 K−1, and thermal conductance to ambient Gth = 10 W·K−1. At steady state,

Gth∆T = I²R0(1 + αR∆T)

Hence,

∆T = I²R0/(Gth − I²R0αR)
= 200/(10 − 0.78)
≈ 21.7 K

A one-way calculation with fixed resistance gives only 20 K. A finite stable solution in this linear model requires Gth > I²R0αR. Voltage-driven operation can produce different feedback because current falls as resistance rises.

Nonlinear magnetic saturation, radiation proportional to T4, temperature-dependent viscosity, contact changes, and phase transitions can further strengthen coupling.

7. Numerical Solution Strategies

7.1 Sequential one-way solution

The electromagnetic field is solved first, and losses or forces are mapped to thermal or structural meshes. This method is economical when feedback is weak.

7.2 Partitioned iterative solution

Each physics solver remains separate. At coupling iteration k, properties and source terms are exchanged until a convergence measure such as

||Tk+1 − Tk||/||Tk+1|| < εc

is satisfied. Under-relaxation,

Tk+1 ← (1−β)Tk + βTk+1raw, 0 < β ≤ 1

can stabilize strong feedback, although it may slow convergence.

7.3 Monolithic solution

All coupled unknowns are assembled into one nonlinear algebraic system. Monolithic methods can be robust for strongly coupled problems but require more memory, specialized preconditioners, and careful scaling because electric potential, temperature, velocity, and displacement have very different magnitudes and units.

7.4 Mesh and time-scale considerations

  • Resolve skin depth with enough elements to capture steep current gradients.
  • Refine air gaps, corners, contacts, thermal boundary layers, and fluid near-wall regions.
  • Use electromagnetic cycle averaging only when thermal and mechanical variables change negligibly during one cycle.
  • Test mesh, timestep, nonlinear, and coupling convergence separately.
  • Conservatively map total loss, force, and heat flux between nonmatching meshes.

7.5 Verification and validation

Verification asks whether the equations were solved correctly. It includes benchmark comparison, conservation checks, and refinement studies. Validation asks whether the chosen equations adequately represent reality. It requires measurements such as temperature, torque, impedance, flow rate, vibration, or magnetic flux.

Energy consistency can be checked using Poynting's theorem:

∂uEM/∂t + ∇ · S = −J · E

For linear nondispersive vacuum, uEM = ½(ε0|E|² + |B|²/μ0) and S = E × H. In dispersive materials, electromagnetic stored-energy expressions require a constitutively appropriate treatment.

8. Contemporary Applications

ApplicationPrincipal couplingsMajor design concern
Electric machinesEM–thermal–fluid–structuraltorque density, hotspot, vibration
Induction heatingEM–thermal–phase transformationpenetration and temperature uniformity
TransformersEM–thermal–fluid–acousticinsulation ageing and noise
Wireless powerfull-wave EM–thermalefficiency, alignment, exposure
MRI systemsEM–thermal–mechanicalquench, force, patient safety
Power electronicsEM–thermal–mechanicalparasitics, junction temperature, fatigue
Plasma processingEM–plasma–fluid–chemicalnon-equilibrium transport and uniformity
MagnetohydrodynamicsEM–fluid–thermalLorentz-force control and Joule heating
BioelectromagneticsEM–thermal–biologicalspecific absorption and tissue safety

8.1 Reduced-order models and AI

Proper orthogonal decomposition, equivalent thermal networks, response surfaces, and neural surrogate models can reduce computational cost for optimization or real-time control. However, an AI surrogate is reliable only within its validated parameter domain. Training data should satisfy conservation laws and cover nonlinear regimes such as saturation and thermal runaway. Physics-informed models can embed governing equations but do not eliminate the need for independent validation and uncertainty assessment.

8.2 Digital twins

A digital twin combines a model with operational measurements. In an electrical machine, measured current, coolant temperature, and vibration may update estimates of rotor temperature or demagnetization risk. Observability, sensor calibration, cybersecurity, model drift, and uncertainty reporting are essential.

9. Applied Case: Liquid-Cooled Electric-Vehicle Motor

This is an illustrative engineering case rather than a report of a commercial product.

Background

A high-speed permanent-magnet motor is required to deliver repeated peak-power operation. The design includes stator windings, a laminated core, magnets, an air gap, a water–glycol cooling jacket, and a structural housing.

Problem

A preliminary electromagnetic model predicts acceptable torque, but a one-way thermal calculation estimates a winding hotspot of 172 °C, above the 155 °C insulation design limit. The model also ignores temperature-dependent copper resistance, magnet remanence, coolant advection, and thermally induced air-gap changes.

Analysis

The electromagnetic model supplies spatially resolved copper, core, magnet eddy-current, and mechanical-loss inputs. The coolant is modeled using incompressible flow and the moving-fluid energy equation, including ρcpu·∇T. The solid regions use heat conduction. Winding conductivity and magnet properties are updated with temperature.

The electromagnetic force harmonics are transferred to a structural model. Maxwell stress is cycle-averaged over a closed air-gap surface in periodic steady state; under this condition the average electromagnetic momentum-storage term vanishes. Modal analysis identifies whether force harmonics approach housing resonances.

Approach

  1. Perform mesh-convergence studies in the air gap, conductors, and coolant boundary layers.
  2. Solve electromagnetic and fluid fields at selected operating points.
  3. Map losses conservatively to the thermal mesh.
  4. Iterate temperature-dependent properties until loss and hotspot changes are below prescribed tolerances.
  5. Optimize cooling-channel position, conductor arrangement, and switching harmonics.
  6. Validate losses with electrical input–output measurements and validate temperature using embedded sensors.

Illustrative outcome

After increasing coolant-side area and reducing proximity loss through conductor rearrangement, the converged model predicts a 149 °C hotspot at the design operating condition. The revised solution also shows a 6% increase in copper loss relative to the original fixed-temperature electromagnetic calculation. A problematic radial force harmonic is reduced by modifying the current waveform. These values are illustrative outputs of the stated scenario, not experimentally established universal results.

Learning points

  • A torque-compliant design may still fail thermally or mechanically.
  • Coolant advection must be represented when flow is resolved.
  • Loss mapping should preserve integrated power.
  • Temperature-dependent electromagnetic properties can materially change results.
  • Cycle-averaged Maxwell stress is appropriate only under periodic steady-state conditions.
  • Validation should use multiple independent observables.

10. Engineering Challenges and Best Practices

Challenges

  1. Constitutive uncertainty: magnetic hysteresis, contact resistance, turbulence, and anisotropic composites may be poorly characterized.
  2. Scale separation: electromagnetic, acoustic, mechanical, and thermal timescales may differ by many orders of magnitude.
  3. Geometric uncertainty: small air-gap or contact-pressure changes can produce large effects.
  4. Numerical stiffness: strong feedback may destabilize partitioned iterations.
  5. Measurement limitations: internal hotspot, stress, and current density are difficult to observe directly.
  6. Model-form error: simplified turbulence, loss, or homogenization models may dominate discretization error.

Recommended practice

  • State every neglected term and justify it quantitatively.
  • Use dimensionless numbers to identify dominant transport mechanisms.
  • Distinguish peak, RMS, instantaneous, and cycle-averaged quantities.
  • Confirm that phasor conventions match loss formulas.
  • Apply Maxwell stress on suitable surfaces and account for field momentum in transients.
  • Conduct sensitivity and uncertainty analyses, not only nominal simulations.
  • Use conservative interpolation between meshes.
  • Validate under normal, overload, startup, and fault conditions.

11. Safety, Ethics, Governance, and Regulation

Multiphysics errors can cause insulation breakdown, fire, excessive electromagnetic exposure, mechanical rupture, coolant leakage, or unsafe medical-device operation. Engineers should document assumptions, calibration data, uncertainty bounds, software versions, and model limitations.

Applicable requirements depend on sector and jurisdiction, but may include electromagnetic compatibility, human exposure, machinery safety, insulation coordination, pressure-system, medical-device, and functional-safety standards. Compliance testing does not replace engineering analysis, and simulation does not replace mandated testing.

AI-assisted optimization must not conceal unsafe extrapolation. Proprietary data, digital-twin telemetry, and patient or operator data require appropriate privacy and cybersecurity controls. Professional responsibility requires communicating credible worst-case outcomes rather than only favorable nominal predictions.

Chapter Summary

Multiphysics electromagnetic engineering integrates Maxwell equations with thermal transport, fluid mechanics, and structural dynamics. Electromagnetic losses provide heat sources, fields produce forces and torque, moving fluids advect heat, and temperature or deformation feeds back through material properties and geometry. The moving-fluid energy equation must include the advective term. Maxwell-stress surface integration alone is justified for static or quasistatic conditions, or after cycle averaging in periodic steady state; general transient force also includes electromagnetic momentum storage.

Accurate analysis depends on valid constitutive models, interface conditions, mesh and timestep convergence, conservative data transfer, and experimental validation. Sequential coupling is efficient for weak feedback, whereas iterative partitioned or monolithic methods are needed for strongly coupled systems. Contemporary applications increasingly use reduced-order models, AI surrogates, and digital twins, but these tools require domain control, uncertainty assessment, governance, and physical validation.

Key Terms

Advection: Transport of thermal energy by bulk fluid motion.

Constitutive law: Relationship connecting field variables to material response.

Cycle averaging: Averaging a periodic quantity over one complete period.

Digital twin: A computational representation updated using operational data.

Eddy current: Current induced in a conductor by a time-varying magnetic field.

Electromagnetic momentum: Momentum stored in electromagnetic fields.

Electrothermal feedback: Mutual interaction between electrical loss and temperature.

Fluid–structure interaction: Coupling between fluid forces and structural motion.

Joule heating: Irreversible electrical power density J·E.

Lorentz force: Force on free charge and current due to electric and magnetic fields.

Magnetic Reynolds number: Ratio characterizing magnetic induction by motion to magnetic diffusion.

Maxwell stress tensor: Tensor describing electromagnetic momentum flux and stress.

Monolithic coupling: Simultaneous solution of all coupled field unknowns.

Partitioned coupling: Iterative exchange between separate physics solvers.

Péclet number: Ratio of advective to conductive thermal transport.

Skin depth: Characteristic electromagnetic penetration depth in a good conductor.

Thermoelasticity: Mechanical deformation and stress caused partly by temperature change.

Validation: Assessment of whether a model adequately represents physical reality.

Verification: Assessment of whether equations have been solved correctly.

Review Questions

Short Answer Questions

  1. Distinguish one-way, weak, and strong multiphysics coupling.
  2. Why must advective transport be included in a moving-fluid thermal model?
  3. State the conditions under which Maxwell-stress surface integration alone gives the total force.
  4. What physical information is provided by the thermal Péclet number?
  5. Why should loss transfer between nonmatching meshes be conservative?

Long Answer Questions

  1. Derive the magnetic-vector-potential equation for an eddy-current conductor and state its assumptions.
  2. Explain electromagnetic–thermal feedback in a current-driven coil and discuss thermal stability.
  3. Develop the governing equations and interface conditions for a liquid-cooled electrical machine.
  4. Compare sequential, partitioned iterative, and monolithic solution strategies.
  5. Discuss verification, validation, and uncertainty quantification for multiphysics electromagnetic simulations.

Analytical / Application Questions

  1. A conducting plate is heated inductively while moving through a cooling liquid. Formulate a coupled model, identify all source terms, and propose appropriate boundary conditions.
  2. Develop a method for calculating transient force on a body using Maxwell stress and electromagnetic momentum. Explain when cycle averaging is permissible.
  3. Design a validation programme for an AI-assisted digital twin of a transformer, including measurements, uncertainty metrics, cybersecurity controls, and limits on extrapolation.

Multiple Choice Questions with Answers

Question 1

Which coupling correctly represents convective or advective heat transport in a resolved cooling system?

A. Mechanical field to fluid field

B. Fluid velocity field to thermal field

C. Thermal field to electromagnetic momentum only

D. Electromagnetic field to structural strain only

Correct Answer: B. Fluid velocity field to thermal field

Question 2

When may total force be obtained from the Maxwell-stress surface integral without an explicit electromagnetic momentum-storage term?

A. For every electromagnetic transient

B. Only when material permeability equals zero

C. In static or quasistatic conditions with negligible momentum storage, or as a periodic steady-state cycle average

D. Only inside a perfect conductor

Correct Answer: C. In static or quasistatic conditions with negligible momentum storage, or as a periodic steady-state cycle average

Question 3

Which term represents thermal advection in an incompressible moving fluid?

A. ρcpu·∇T

B. ∇·B

C. μσUL

D. ½ε|E|2

Correct Answer: A. ρcpu·∇T

Question 4

For copper with σ=5.8×107 S·m-1 and μ=μ0 at 100 kHz, the good-conductor skin depth is approximately:

A. 0.0209 mm

B. 0.209 mm

C. 2.09 mm

D. 20.9 mm

Correct Answer: B. 0.209 mm

Question 5

A fluid has ρ=997 kg·m-3, cp=4180 J·kg-1·K-1, and u=0.20 m·s-1. For uniform heating q=2.0×106 W·m-3 over 0.50 m, with axial conduction and wall losses neglected, what is the temperature rise?

A. 0.12 K

B. 0.60 K

C. 1.20 K

D. 12.0 K

Correct Answer: C. 1.20 K

Question 6

Which dimensionless number compares advective thermal transport with thermal conduction?

A. Magnetic Reynolds number

B. Péclet number

C. Mach number

D. Weber number

Correct Answer: B. Péclet number

Question 7

Which numerical strategy is generally most appropriate when field feedback is strong and sequential one-way transfer is inaccurate?

A. A partitioned iterative or monolithic solution

B. A fixed-property electromagnetic solution only

C. Elimination of all interface conditions

D. A single analytical skin-depth calculation

Correct Answer: A. A partitioned iterative or monolithic solution

Question 8

For sinusoidal steady state represented by peak phasors, the average Joule-loss density is:

A. Re\{J·E^*\}

B. ½Re\{J·E^*\}

C. ½J×B

D. ωμ|H|

Correct Answer: B. ½Re\{J·E^*\}

Question 9

In the current-driven coil example, what steady temperature rise results from I=100 A, R0=0.020 Ω, αR=0.0039 K-1, and Gth=10 W·K-1?

A. 10.0 K

B. 20.0 K

C. 21.7 K

D. 78.0 K

Correct Answer: C. 21.7 K

Question 10

When a coolant domain is explicitly resolved using fluid and energy equations, the solid–fluid wall should normally use:

A. An empirical convection coefficient in addition to continuity of heat flux

B. Zero temperature on both sides

C. Continuity of temperature and normal heat flux without double-counting convection

D. A magnetic insulation condition as the thermal boundary condition

Correct Answer: C. Continuity of temperature and normal heat flux without double-counting convection

Electro Magnetic Field
Chapter 14 of 14