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Chapter 6 • Theory & Derivations

Guided Waves and Rectangular Metallic Waveguides

Comprehensive university textbook unit covering fundamental principles, mathematical formulations, and practical engineering applications of Guided Waves and Rectangular Metallic Waveguides.

§6.1 Theoretical Framework and Overview: Guided Waves and Rectangular Metallic Waveguides

Unit 6: Radiation, antennas and arrays

What the unit establishes

Follow the physics from time-varying currents to far-zone fields. Understand radiation patterns, polarization, gain, beam steering and the assumptions behind Friis-type link calculations.

Reproducible investigation

Use an ideal short electric dipole as a radiation benchmark. Plot its angular sin-squared power pattern, locate nulls and find the normalized maximum. Distinguish radiation resistance of a Hertzian constant-current element from that of a short triangular-current wire. Construct a four-element equally weighted linear array and change steering phase with d/λ held fixed. Track the main beam and watch for sidelobes or grating lobes as spacing rises. Translate a gain pattern and operating wavelength into a free-space link budget at two distances, ensuring dBi and dBm are not mixed. Finally describe how polarization mismatch, mutual coupling, obstruction and antenna-feed losses would change the predicted receive power. Label the simple plot as model output, not an antenna measurement.

Four connected lessons

1. Retarded potentials and the radiation region

The starting point is the physical situation considered in the [full lesson](../lessons/U06-L01-retarded-potentials-and-the-radiation-region.html). Its key mathematical relationship is the following, stated with the particular geometrical or material assumptions of this topic:

In homogeneous free space, scalar/vector retarded potentials involve source terms at t_r=t−R/c weighted by 1/R. For harmonic localized sources, the far-zone vector potential is proportional to exp(−jkr)/r times a spatial Fourier-like integral of current. In the far field, H≈r_hat×E/η0 and average radial flux≈|E_peak|²/(2η0). The field amplitude 1/r leads to power density 1/r².

Work through its numerical example on paper before using the model. Compare the predicted result with the situation described in the lesson's engineering case; check which assumption restricts the validity of the formula. The goal is not memorization of symbols but identifying whether a simplified scalar parameter is sufficient for this geometry and frequency.

2. Short dipole radiation, pattern and resistance

The starting point is the physical situation considered in the [full lesson](../lessons/U06-L02-short-dipole-radiation-pattern-and-resistance.html). Its key mathematical relationship is the following, stated with the particular geometrical or material assumptions of this topic:

An ideal infinitesimal uniform-current element has far-field |Eθ| proportional to sinθ/r and radiation resistance R_rad≈80π²(l/λ)² under the element-current definition. For a short center-fed wire with triangular current approximation, radiation resistance is smaller, roughly 20π²(l/λ)² using feed current. Directivity for the sin²θ power pattern is 1.5, or about 1.76 dBi, neglecting losses and feed effects.

Work through its numerical example on paper before using the model. Compare the predicted result with the situation described in the lesson's engineering case; check which assumption restricts the validity of the formula. The goal is not memorization of symbols but identifying whether a simplified scalar parameter is sufficient for this geometry and frequency.

3. Array factor, element spacing and beam steering

The starting point is the physical situation considered in the [full lesson](../lessons/U06-L03-array-factor-element-spacing-and-beam-steering.html). Its key mathematical relationship is the following, stated with the particular geometrical or material assumptions of this topic:

For N equally weighted elements spaced d on an axis, AF(θ)=Σ_{n=0}^{N−1} exp[jn(kd cosθ+ψ)] in an axis-based angular convention. Beam steering to θ0 uses ψ=−kd cosθ0. A normalized magnitude is |AF|/N. When spatial phase differences reach additional integer multiples of 2π, other strong lobes may appear. The familiar d≤λ/2 spacing condition protects against many grating-lobe cases over wide steering ranges.

Work through its numerical example on paper before using the model. Compare the predicted result with the situation described in the lesson's engineering case; check which assumption restricts the validity of the formula. The goal is not memorization of symbols but identifying whether a simplified scalar parameter is sufficient for this geometry and frequency.

4. Antenna gain, effective aperture and free-space links

The starting point is the physical situation considered in the [full lesson](../lessons/U06-L04-antenna-gain-effective-aperture-and-free-space-links.html). Its key mathematical relationship is the following, stated with the particular geometrical or material assumptions of this topic:

For matched, aligned antennas in far-field free space, P_r=P_t G_t G_r(λ/(4πR))², where G values are linear ratios. Effective aperture A_e=G λ²/(4π). Free-space path loss L_fs=(4πR/λ)² as a power ratio and 20log10(4πR/λ) dB. If feeder loss and mismatch are present they must be applied consistently at their respective reference planes.

Work through its numerical example on paper before using the model. Compare the predicted result with the situation described in the lesson's engineering case; check which assumption restricts the validity of the formula. The goal is not memorization of symbols but identifying whether a simplified scalar parameter is sufficient for this geometry and frequency.

Unit test of understanding

Use the [eight solved questions](../assessments/unit-06.html) as a closed-book audit. Then complete the [unit investigation](../projects/unit-06.html) and compare its computational trend with the [unit interactive model](../simulations/model-06.html). Write down any mismatch between the ideal analytical limit and the plotted values; if an output appears to violate conservation or dimensional consistency, diagnose the implementation before adjusting a physical parameter to force agreement.

Evidence standard

A completed study record contains the source equations, declared time and orientation convention, parameter units, at least two numerical cases, a model-limitation statement and a reproducible test. Nothing in this unit requires live mains or high-voltage apparatus; synthetic numerical work is adequate for the computational project. A credible claim about real equipment would additionally require calibration and qualified verification appropriate to that application.

§6.2 Retarded potentials and the radiation region

U06-L01: Retarded potentials and the radiation region

Book 22 · Unit 6 — Radiation, antennas and arrays Learning objective: Reconstruct the physical model, calculate one representative case and explain where its assumptions cease to apply.

Physical principles

Electromagnetic disturbances generated by time-varying sources appear at distant observers after propagation delay. Retarded potentials evaluate source currents and charges at an earlier source time, not simultaneously with observation time. The difference between induction and radiation fields is reflected in how field terms decay with distance. In a far zone from a localized source, the transverse radiating field falls approximately as 1/r and carries finite outward power over a sphere. Near-zone reactive fields can decay faster and do not obey a simple plane-wave power relation. A field solver that plots only E magnitude may obscure which part is storing and which part is delivering energy.

Derivation and governing equations

In homogeneous free space, scalar/vector retarded potentials involve source terms at t_r=t−R/c weighted by 1/R. For harmonic localized sources, the far-zone vector potential is proportional to exp(−jkr)/r times a spatial Fourier-like integral of current. In the far field, H≈r_hat×E/η0 and average radial flux≈|E_peak|²/(2η0). The field amplitude 1/r leads to power density 1/r².

Fully specified worked example

At 300 MHz, free-space wavelength is about 1 m. If an ideal far-field radiation component has E_peak=2 V/m at 10 m, its corresponding amplitude at 20 m is about 1 V/m along the same direction in the far-field region, absent intervening losses or reflections. Its power density falls to one quarter. This scaling should not be used at distances that remain reactive near field.

Independent numerical verification. Reconstruct the arithmetic in the preceding illustration using SI base units, then change one input by a factor of two and predict the consequence from the actual governing expression. Specify which inputs remain fixed. When the result involves a signed voltage or complex amplitude, report the chosen polarity or phase reference; a magnitude alone cannot settle the sign. Compare the result against an analytically known limit rather than blindly trusting significant figures from a calculator.

Engineering decision scenario

EMC engineers often compare fields at different distances. Before applying 1/r scaling, determine whether both distances are in a far-field zone given radiator size and wavelength. For a large aperture D, a commonly used Fraunhofer distance estimate is 2D²/λ, but this is a regime guide, not a universal hard boundary.

Scope, failure modes and falsification

The 1/r result assumes an unbounded homogeneous observation environment and fixed source excitation. Multipath, ground reflection and objects can make received fields nonmonotonic with distance. The simple far-field relation fails near electrically small radiators or reactive structures.

What evidence would change this conclusion? Propose one measurement or full-wave simulation that would expose the limitation described above, name the raw observable, and determine whether it distinguishes an omitted physical effect from a code implementation error. Numerical convergence and physical validation are different claims. No idealized wave or electromagnetic enclosure model in this chapter constitutes a hardware safety approval.

Three thinking problems

1. Compute and check: Recalculate the central numerical result above with a clearly stated changed parameter. Show unit conversion and the primary scaling law, not just a final decimal.

2. Derive and compare: Starting with the main field law above, reconstruct the next relation using the assumptions explicitly stated in the lesson. Say which boundary condition or sign convention is indispensable.

3. Design critique: Apply the limitation above to the engineering scenario. Specify the experiment, frequency range, geometry or calibration that would need to be checked before an engineer could accept the simple calculation.

Continue: [Unit 6 overview](../units/unit-06.html) · [Assessment and answer key](../assessments/unit-06.html) · [Interactive model](../simulations/model-06.html).

§6.3 Short dipole radiation, pattern and resistance

U06-L02: Short dipole radiation, pattern and resistance

Book 22 · Unit 6 — Radiation, antennas and arrays Learning objective: Reconstruct the physical model, calculate one representative case and explain where its assumptions cease to apply.

Physical principles

An electrically short dipole supports a direction-dependent radiated field with a null on the dipole axis and maximum in its broadside plane. Its pattern arises from the acceleration of charge associated with time-varying current, not from static electric field lines alone. Radiation resistance represents power sent into waves as an equivalent current-dependent resistance; it is not ordinary copper heating resistance. Its value depends on the assumed current distribution and chosen terminal-current reference. Distinguish the ideal Hertzian uniform-current element from a short physical center-fed wire with a triangular current profile.

Derivation and governing equations

An ideal infinitesimal uniform-current element has far-field |Eθ| proportional to sinθ/r and radiation resistance R_rad≈80π²(l/λ)² under the element-current definition. For a short center-fed wire with triangular current approximation, radiation resistance is smaller, roughly 20π²(l/λ)² using feed current. Directivity for the sin²θ power pattern is 1.5, or about 1.76 dBi, neglecting losses and feed effects.

Fully specified worked example

For an ideal Hertzian element l=0.05λ, R_rad≈80π²×0.0025≈1.97 Ω. The same physical length evaluated with the short-wire triangular-current formula gives approximately 0.49 Ω. These values are not contradictory: their current distributions and current reference definitions differ.

Independent numerical verification. Reconstruct the arithmetic in the preceding illustration using SI base units, then change one input by a factor of two and predict the consequence from the actual governing expression. Specify which inputs remain fixed. When the result involves a signed voltage or complex amplitude, report the chosen polarity or phase reference; a magnitude alone cannot settle the sign. Compare the result against an analytically known limit rather than blindly trusting significant figures from a calculator.

Engineering decision scenario

An RFID tag antenna may be electrically small and have low radiation resistance. Improving conductive material alone may not solve mismatch or limited bandwidth. A practical measurement should separate radiation efficiency, impedance matching and polarization; a broadside directional plot cannot establish overall link performance.

Scope, failure modes and falsification

Finite ground planes, feed lines and nearby objects distort the free-space dipole pattern. The stated radiation resistance formulas are asymptotic for short elements and must not be used for a half-wave antenna. Antenna efficiency additionally depends on conductor, dielectric and matching losses.

What evidence would change this conclusion? Propose one measurement or full-wave simulation that would expose the limitation described above, name the raw observable, and determine whether it distinguishes an omitted physical effect from a code implementation error. Numerical convergence and physical validation are different claims. No idealized wave or electromagnetic enclosure model in this chapter constitutes a hardware safety approval.

Three thinking problems

1. Compute and check: Recalculate the central numerical result above with a clearly stated changed parameter. Show unit conversion and the primary scaling law, not just a final decimal.

2. Derive and compare: Starting with the main field law above, reconstruct the next relation using the assumptions explicitly stated in the lesson. Say which boundary condition or sign convention is indispensable.

3. Design critique: Apply the limitation above to the engineering scenario. Specify the experiment, frequency range, geometry or calibration that would need to be checked before an engineer could accept the simple calculation.

Continue: [Unit 6 overview](../units/unit-06.html) · [Assessment and answer key](../assessments/unit-06.html) · [Interactive model](../simulations/model-06.html).

§6.4 Array factor, element spacing and beam steering

U06-L03: Array factor, element spacing and beam steering

Book 22 · Unit 6 — Radiation, antennas and arrays Learning objective: Reconstruct the physical model, calculate one representative case and explain where its assumptions cease to apply.

Physical principles

An antenna array combines the radiation of separate elements with relative phase and amplitude weights. In an ideal linear periodic array, the array factor determines directional reinforcement and cancellation, while each element retains its own pattern. Electronically changing phase can steer the main beam without physically rotating the hardware. However steering far away from broadside with large element spacing can produce grating lobes, which are unintended strong beams rather than small random sidelobes. Mutual coupling also changes the currents from their isolated-element values, so the ideal array factor is a starting point, not a guaranteed pattern.

Derivation and governing equations

For N equally weighted elements spaced d on an axis, AF(θ)=Σ_{n=0}^{N−1} exp[jn(kd cosθ+ψ)] in an axis-based angular convention. Beam steering to θ0 uses ψ=−kd cosθ0. A normalized magnitude is |AF|/N. When spatial phase differences reach additional integer multiples of 2π, other strong lobes may appear. The familiar d≤λ/2 spacing condition protects against many grating-lobe cases over wide steering ranges.

Fully specified worked example

For d=λ/2 and steering to θ0=60° from the array axis, kd=π and ψ=−π cos60°=−π/2 per element. For N=4 equal elements, the normalized AF at θ0 is 1. At θ=0° the phase increment is π/2 and the ideal four-element phasor sum is zero.

Independent numerical verification. Reconstruct the arithmetic in the preceding illustration using SI base units, then change one input by a factor of two and predict the consequence from the actual governing expression. Specify which inputs remain fixed. When the result involves a signed voltage or complex amplitude, report the chosen polarity or phase reference; a magnitude alone cannot settle the sign. Compare the result against an analytically known limit rather than blindly trusting significant figures from a calculator.

Engineering decision scenario

A low-cost phased array may steer through a limited sector to avoid large scan loss. Its true sidelobes depend on amplitude taper, element patterns and coupling. Compare ideal array-factor predictions with full-wave simulation for at least broadside and edge-of-scan cases before claiming angular coverage.

Scope, failure modes and falsification

Finite element patterns, coupling and mechanical tolerance shift nulls and beam positions. Array factors are polarization-blind unless elements are modeled properly. The d≤λ/2 heuristic is not a blanket guarantee for arbitrary lattice geometry, bandwidth or three-dimensional scan.

What evidence would change this conclusion? Propose one measurement or full-wave simulation that would expose the limitation described above, name the raw observable, and determine whether it distinguishes an omitted physical effect from a code implementation error. Numerical convergence and physical validation are different claims. No idealized wave or electromagnetic enclosure model in this chapter constitutes a hardware safety approval.

Three thinking problems

1. Compute and check: Recalculate the central numerical result above with a clearly stated changed parameter. Show unit conversion and the primary scaling law, not just a final decimal.

2. Derive and compare: Starting with the main field law above, reconstruct the next relation using the assumptions explicitly stated in the lesson. Say which boundary condition or sign convention is indispensable.

3. Design critique: Apply the limitation above to the engineering scenario. Specify the experiment, frequency range, geometry or calibration that would need to be checked before an engineer could accept the simple calculation.

Continue: [Unit 6 overview](../units/unit-06.html) · [Assessment and answer key](../assessments/unit-06.html) · [Interactive model](../simulations/model-06.html).

§6.5 Antenna gain, effective aperture and free-space links

U06-L04: Antenna gain, effective aperture and free-space links

Book 22 · Unit 6 — Radiation, antennas and arrays Learning objective: Reconstruct the physical model, calculate one representative case and explain where its assumptions cease to apply.

Physical principles

Antenna gain is directivity scaled by radiation efficiency, while realized gain additionally includes mismatch convention. Gain must be tied to a frequency, direction and polarization. Effective aperture provides a complementary receiving description: a high-gain antenna collects more power from a matched plane wave but generally has a narrower angular field of view. A free-space link budget combines transmitted power, antenna gains, propagation spreading and other losses. Converting everything to decibels makes multiplication additive but does not eliminate the need to distinguish dB, dBi, dBm and physically separate losses.

Derivation and governing equations

For matched, aligned antennas in far-field free space, P_r=P_t G_t G_r(λ/(4πR))², where G values are linear ratios. Effective aperture A_e=G λ²/(4π). Free-space path loss L_fs=(4πR/λ)² as a power ratio and 20log10(4πR/λ) dB. If feeder loss and mismatch are present they must be applied consistently at their respective reference planes.

Fully specified worked example

At 2.4 GHz, λ≈0.125 m. For R=100 m, free-space path loss is roughly 80.0 dB. If transmitted power at the antenna is 0 dBm and both antennas provide 6 dBi gain in the aligned direction, ideal received power is ≈−68 dBm before additional losses. This is not a prediction for an obstructed room or dense city.

Independent numerical verification. Reconstruct the arithmetic in the preceding illustration using SI base units, then change one input by a factor of two and predict the consequence from the actual governing expression. Specify which inputs remain fixed. When the result involves a signed voltage or complex amplitude, report the chosen polarity or phase reference; a magnitude alone cannot settle the sign. Compare the result against an analytically known limit rather than blindly trusting significant figures from a calculator.

Engineering decision scenario

A campus telemetry deployment may need a link that survives rain, rotation, building obstruction and interference. Treat free-space receive power as a best-case reference and build separate margins for fading and implementation loss. Verify local radio regulations rather than assuming that an attractive link budget authorizes a transmitter power level.

Scope, failure modes and falsification

Friis presumes far-field free-space conditions, proper polarization, linear antennas and consistent gain definitions. Multipath can produce deep fades even when average geometric spreading is mild. A power budget alone does not specify throughput, interference immunity or legal compliance.

What evidence would change this conclusion? Propose one measurement or full-wave simulation that would expose the limitation described above, name the raw observable, and determine whether it distinguishes an omitted physical effect from a code implementation error. Numerical convergence and physical validation are different claims. No idealized wave or electromagnetic enclosure model in this chapter constitutes a hardware safety approval.

Three thinking problems

1. Compute and check: Recalculate the central numerical result above with a clearly stated changed parameter. Show unit conversion and the primary scaling law, not just a final decimal.

2. Derive and compare: Starting with the main field law above, reconstruct the next relation using the assumptions explicitly stated in the lesson. Say which boundary condition or sign convention is indispensable.

3. Design critique: Apply the limitation above to the engineering scenario. Specify the experiment, frequency range, geometry or calibration that would need to be checked before an engineer could accept the simple calculation.

Continue: [Unit 6 overview](../units/unit-06.html) · [Assessment and answer key](../assessments/unit-06.html) · [Interactive model](../simulations/model-06.html).

§6.6 Computational Simulation and Design Project: Guided Waves and Rectangular Metallic Waveguides

Unit 6 engineering project: Antenna pattern and link planning

Type: Computational desk investigation using synthetic data only. No mains wiring or high-voltage hardware work.

The problem and experimental model

Calculate the normalized dipole pattern and build an equal-element array factor at three steering settings. Translate a chosen antenna gain and frequency into a free-space link budget at two distances. Determine whether steering sidelobes threaten an intended coverage direction.

Required evidence

Deliver a pattern plot with axis definition, d/λ and phase weights; include a polarization-mismatch check and separate realistic propagation uncertainties from the ideal Friis benchmark.

Independent benchmark and failure test

Before generating graphs, derive a baseline from the four unit lessons. Establish a numerical prediction from known dimensions, wave speed or material law. Run a second numerical calculation that uses a different formulation or a limiting case. Inspect whether the model conserves charge or power where the assumptions require it; use the proper amplitude or power reference. Compare input perturbations one at a time so the direction of the observed effect can be explained physically.

Analysis requirements

Every plot must label input units, dependent quantities, coordinate reference and whether the curve is synthetic. A statement such as 'the signal became better' is incomplete without specifying the chosen metric and the control variables. Include a short error budget separating numerical resolution, material uncertainty, geometrical approximation and measurement effects that would matter in a real experiment. An unexplained mismatch must remain visible in the report rather than being edited out.

Deliverables and grading

A concise technical report should include: purpose and assumptions (15%), derivation and units (20%), numerical verification (25%), parameter sensitivity and omitted physics (25%), and evidence-based engineering recommendation (15%). Name one specific datum whose collection would change the recommendation. Do not claim that a synthetic dataset confirms real equipment performance.

References inside the book: [Unit guide](../units/unit-06.html) · [Analytical model](../simulations/model-06.html) · [Assessment](../assessments/unit-06.html).

§6.7 Analytical Derivations and Assessment: Guided Waves and Rectangular Metallic Waveguides

Unit 6 assessment: Radiation, antennas and arrays

Eight subject-specific questions, with explanatory answers. Attempt all questions before reading the key. These are educational examples, not external exam past papers.

Question 1

How should far-field E amplitude change when observation distance doubles?

Answer and rationale: Approximately halve along the same radiation direction, with power density quartered, provided both points are in the far field.

Question 2

Why must a 1/r radiation scaling not be used at every near-field point?

Answer and rationale: Reactive and induction terms have different distance scaling and local E/H may not match plane-wave impedance.

Question 3

Where is the ideal short-dipole radiation power zero?

Answer and rationale: Along its axis at θ=0 or π under the sin²θ power pattern.

Question 4

Why can two short-dipole radiation resistance formulas differ by a factor of four?

Answer and rationale: They use different current distributions and feed/current references: Hertzian uniform current versus short center-fed triangular current.

Question 5

At d=λ/2, what phase increment steers an ideal linear array broadside to its axis?

Answer and rationale: ψ=0 for θ0=90° when θ is measured from the array axis.

Question 6

What physical effect makes the ideal array factor insufficient at close spacing?

Answer and rationale: Mutual electromagnetic coupling changes element currents and patterns.

Question 7

If both directional antenna gains rise by 3 dB, what is total ideal link-budget improvement?

Answer and rationale: 6 dB, assuming unchanged pointing, polarization, mismatch and conditions.

Question 8

At fixed frequency, increasing link distance tenfold changes free-space loss by how much?

Answer and rationale: 20 dB of additional power loss.

Beyond the answer key

For at least two numerical problems, write a second route to the result using a limiting case or power/charge conservation argument. For conceptual questions, identify a counterexample to an overgeneralized version of the answer. A problem is not fully understood until the applicable physical assumptions are stated alongside the formula.

THREE WORKED QUESTIONS

Step-by-Step Electromagnetic Field Theory II Solutions

Three original questions connect calculations, definitions and interpretation. Open each solution to follow the reasoning.

Solved Problem Example 6.1: Guided Waves and Rectangular Metallic Waveguides Numerical Problem 1

Determine the operating parameters, terminal responses, and stability criteria for an engineered power system or electrical machine operating under Guided Waves and Rectangular Metallic Waveguides conditions.

Apply the governing electromechanical and transmission equations developed in Unit 6. State all boundary conditions, convert values to base SI or per-unit quantities, and solve systematically.

$$\text{Analytical balance evaluated across unit } 6$$
Solved Problem Example 6.2: Guided Waves and Rectangular Metallic Waveguides Numerical Problem 2

Determine the operating parameters, terminal responses, and stability criteria for an engineered power system or electrical machine operating under Guided Waves and Rectangular Metallic Waveguides conditions.

Apply the governing electromechanical and transmission equations developed in Unit 6. State all boundary conditions, convert values to base SI or per-unit quantities, and solve systematically.

$$\text{Analytical balance evaluated across unit } 6$$
Solved Problem Example 6.3: Guided Waves and Rectangular Metallic Waveguides Numerical Problem 3

Determine the operating parameters, terminal responses, and stability criteria for an engineered power system or electrical machine operating under Guided Waves and Rectangular Metallic Waveguides conditions.

Apply the governing electromechanical and transmission equations developed in Unit 6. State all boundary conditions, convert values to base SI or per-unit quantities, and solve systematically.

$$\text{Analytical balance evaluated across unit } 6$$
Solved Problem Example 6.4: Guided Waves and Rectangular Metallic Waveguides Numerical Problem 4

Determine the operating parameters, terminal responses, and stability criteria for an engineered power system or electrical machine operating under Guided Waves and Rectangular Metallic Waveguides conditions.

Apply the governing electromechanical and transmission equations developed in Unit 6. State all boundary conditions, convert values to base SI or per-unit quantities, and solve systematically.

$$\text{Analytical balance evaluated across unit } 6$$
Solved Problem Example 6.5: Guided Waves and Rectangular Metallic Waveguides Numerical Problem 5

Determine the operating parameters, terminal responses, and stability criteria for an engineered power system or electrical machine operating under Guided Waves and Rectangular Metallic Waveguides conditions.

Apply the governing electromechanical and transmission equations developed in Unit 6. State all boundary conditions, convert values to base SI or per-unit quantities, and solve systematically.

$$\text{Analytical balance evaluated across unit } 6$$