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Light and Doppler — Examples

1 · Prerequisites

2 · Summary

These computations accompany sr-light-and-doppler. The two pure mathematical workups come first in subject matter: the geometry of the phase level sets of a future null wave covector, where the kernel is positive semidefinite with radical the line through k♯ and that line is the only null direction in the wave front (Worked geometry of the phase level sets of a future null wave covector), and a rational frame-data computation whose boost and inverse boost return the original data (Worked frame data of a future null wave covector and its boost).

The model computations use the exact rational values γ=5/4 and β=3/5. The longitudinal cases at s=±e1 give the factors 1/2 and 2 (Worked longitudinal Doppler shift at beta = 3/5); the two transverse protocols give the factors 5/4 and 4/5 and show that a transverse Doppler statement is incomplete until the frame in which transversality holds is named (Worked transverse Doppler protocols at beta = 3/5); and the aberration workup at cos⁡θ=4/5 gives s′=(5/13,12/13,0) with the frequency factor 13/20 (Worked aberration and Doppler shift at beta = 3/5 and cos theta = 4/5). The companion Counterexample: a transverse wave configuration need not have zero Doppler shift turns the two transverse configurations into an exact counterexample to the universal claim that a transverse orientation leaves the frequency unchanged.

The two mathematical examples use affine Minkowski geometry; the other four items are conditional computations inside the adopted ideal plane-wave model. None performs a measurement, reports data or makes an empirical claim, and none may be used as a dependency of another page's content.

3 · Logical flowchart

4 · Definitions, postulates, theorems and proofs

ExampleConstruction: AI-generatedVerification: AI-generatedOpen item page →

Worked longitudinal Doppler shift at beta = 3/5

Physical scope

Worked longitudinal Doppler computation of the ideal plane-wave model at relative speed (3/5)c in the two propagation directions along the boost axis. Conditional on the model; no measurement, statistical inference or empirical claim.

Example

Worked example in the model of sr-light-and-doppler, on the page sr-light-and-doppler-examples. Let x and x′ be inertial charts with x′=B(β)x+b, β=(3/5)e1, so that γ=5/4 and the frame x′ moves with velocity (3/5)c e1 relative to x. Let an ideal plane wave have frame-x data (ω,s) with ω>0 and (a) s=e1, (b) s=−e1. Then Doppler shift and aberration for an ideal plane wave between inertial descriptions gives:

(a) ω′=γ(1−3/5)ω=(5/4)(2/5)ω=ω/2, ν′=ν/2, λ′=2λ and s′=e1: an observer at rest in x′ moving in the direction of propagation reads half the frequency and twice the wavelength.

(b) ω′=γ(1+3/5)ω=(5/4)(8/5)ω=2ω, ν′=2ν, λ′=λ/2 and s′=−e1: an observer at rest in x′ moving opposite to the propagation direction reads twice the frequency and half the wavelength.

In both cases ∣s′∣=1 and ω′>0, in agreement with the general theorem; the verification uses only the exact rational values γ=5/4, 1−3/5=2/5 and 1+3/5=8/5. Scope: a conditional computation in the ideal plane-wave model; no measurement is performed and no empirical claim is made.

Facts & Assumptions

Given: Inertial charts x,x′ with x′=B(β)x+b, β=(3/5)e1; an ideal plane wave with frame-x data (ω,s), ω>0, ∣s∣=1, and s=±e1.

[A1]

Adopted ideal plane-wave model: one ideal monochromatic plane wave with future null wave covector; the rest observers of x and x′ read the frequencies ω and ω′ (Adopted ideal plane-wave and frequency-reading model, Null wave covectors, frame frequency data and the observer frequency of an ideal plane wave).

[L1]

For the chart pair of the Given the theorem gives ω′=γ(1−β⋅s)ω>0, ν′=γ(1−β⋅s)ν, λ′=λ/[γ(1−β⋅s)], ∣s′∣=1, and in the axis case β=be1 the direction formulas s1′=(s1−b)/(1−bs1), s2′=s2/[γ(1−bs1)], s3′=s3/[γ(1−bs1)] (Doppler shift and aberration for an ideal plane wave between inertial descriptions, clauses (i) and (ii)).

[L2]

Longitudinal clause: for s=βhat the factor is γ(1−∣β∣)=(1−∣β∣)/(1+∣β∣) and for s=−βhat it is γ(1+∣β∣)=(1+∣β∣)/(1−∣β∣); here βhat=e1 (Doppler shift and aberration for an ideal plane wave between inertial descriptions, clause (iii)).

[L3]

γ=(1−∣β∣2)−1/2, so for β=(3/5)e1: γ=(1−9/25)−1/2=5/4; and the boost transformation of the frame data is the one of Boost transformation of a future null wave covector and of its frame data (The passive Lorentz boost with parameter beta).

Verification

technique · direct
1.1A1L3given

Setup. Here βhat=e1, ∣β∣=3/5 and γ=(1−9/25)−1/2=(16/25)−1/2=5/4 by [L3]; both witness directions s=±e1 have ∣s∣=1, so the wave is in the model [A1].

2.1step 1.1L1L2

Case (a), s=e1. Then β⋅s=3/5, so [L1] gives ω′=γ(1−3/5)ω=(5/4)(2/5)ω=ω/2 and hence ν′=ω′/(2π)=ν/2 and λ′=c/ν′=2c/ν=2λ; the axis formulas of [L1] with b=3/5, s1=1, s2=s3=0 give s1′=(1−3/5)/(1−3/5)=1 and s2′=s3′=0, so s′=e1; the frequency factor agrees with the longitudinal clause [L2], ω′/ω=(1−3/5)/(1+3/5)=(2/5)/(8/5)=1/2, since s=βhat.

3.1step 1.1L1L2∎

Case (b), s=−e1. Then β⋅s=−3/5, so [L1] gives ω′=γ(1+3/5)ω=(5/4)(8/5)ω=2ω, ν′=2ν and λ′=c/ν′=λ/2; the axis formulas of [L1] with b=3/5, s1=−1 give s1′=(−1−3/5)/(1+3/5)=−1 and s2′=s3′=0, so s′=−e1; the frequency factor agrees with the longitudinal clause [L2], ω′/ω=(1+3/5)/(1−3/5)=(8/5)/(2/5)=2, since s=−βhat. In both cases ω′>0 and ∣s′∣=1 as the theorem asserts. This proves (a) and (b) by exact rational arithmetic; the computation is conditional on the ideal plane-wave model, no measurement is performed and no empirical claim is made; no choice principle is used.

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Worked transverse Doppler protocols at beta = 3/5

Physical scope

Worked comparison of the two transverse Doppler protocols of the ideal plane-wave model at relative speed (3/5)c: gamma in the frame where the wave is transverse to the motion and 1/gamma in the frame where it is transverse in the observer frame. Conditional on the model; no measurement, statistical inference or empirical claim.

Example

Worked example in the model of sr-light-and-doppler, on the page sr-light-and-doppler-examples, showing that the transverse Doppler shift depends on the frame in which transversality is required. Let x and x′ be inertial charts with x′=B(β)x+b, β=(3/5)e1 and γ=5/4, and let an ideal plane wave have frame-x data (ω,s) with ω>0.

(a) If s=e2, so β⋅s=0 and the propagation direction is perpendicular to the relative velocity in x, then Doppler shift and aberration for an ideal plane wave between inertial descriptions gives ω′=γω=(5/4)ω>ω and s′=(−3/5,4/5,0), which has ∣s′∣=1; the frequency read by the x′-rest observer is blue-shifted by the factor 5/4.

(b) If s=(3/5,4/5,0), so β⋅s=9/25=∣β∣2 and equivalently s′⋅e1=0, the propagation direction is perpendicular to the relative velocity in x′, and the theorem gives ω′=γ(1−9/25)ω=(5/4)(16/25)ω=(4/5)ω=ω/γ<ω and s′=e2; the frequency read by the x′-rest observer is red-shifted by the factor 4/5.

In neither case is ω′=ω for the nonzero β, and the two exact factors differ; a statement of a transverse Doppler shift is therefore incomplete until the frame in which the direction is transverse is specified. Scope: a conditional computation in the ideal plane-wave model; no measurement and no empirical claim.

Facts & Assumptions

Given: Inertial charts x,x′ with x′=B(β)x+b, β=(3/5)e1; an ideal plane wave with frame-x data (ω,s), ω>0, ∣s∣=1.

[A1]

Adopted ideal plane-wave model: one ideal monochromatic plane wave with future null wave covector; the rest observers of x and x′ read the frequencies ω and ω′ (Adopted ideal plane-wave and frequency-reading model, Null wave covectors, frame frequency data and the observer frequency of an ideal plane wave).

[L1]

For the chart pair of the Given the theorem gives ω′=γ(1−β⋅s)ω>0 with γ=(1−∣β∣2)−1/2, and in the axis case β=be1 the direction formulas s1′=(s1−b)/(1−bs1), s2′=s2/[γ(1−bs1)], s3′=s3/[γ(1−bs1)] (Doppler shift and aberration for an ideal plane wave between inertial descriptions, clause (i)).

[L2]

Transverse protocols of the theorem: if β⋅s=0 then ω′=γω and this is greater than ω when β≠0; if β⋅s=∣β∣2, equivalently s′⋅βhat=0 for β≠0, then ω′=ω/γ, which is less than ω when β≠0 (Doppler shift and aberration for an ideal plane wave between inertial descriptions, clause (iv)).

[L3]

γ=(1−∣β∣2)−1/2, so for β=(3/5)e1: γ=(16/25)−1/2=5/4, and ∣β∣2=9/25 (The passive Lorentz boost with parameter beta, Boost transformation of a future null wave covector and of its frame data).

Verification

technique · direct
1.1A1L1L2L3

Case (a). Here s=e2 has ∣s∣=1 and β⋅s=(3/5)(0)=0, so the propagation direction is perpendicular to the relative velocity in x, and [L2] gives ω′=γω=(5/4)ω, which is greater than ω because γ=5/4>1 by [L3]; the axis formulas of [L1] with b=3/5, s1=0, s2=1, s3=0 give s1′=(0−3/5)/(1−0)=−3/5, s2′=1/[(5/4)(1−0)]=4/5 and s3′=0, and ∣s′∣2=9/25+16/25=1.

1.2A1L1L2L3

Case (b). Here s=(3/5,4/5,0) has ∣s∣2=9/25+16/25=1 and β⋅s=(3/5)(3/5)=9/25=∣β∣2; by [L2] this is equivalent to s′⋅βhat=0 with βhat=e1, the propagation direction is perpendicular to the relative velocity in x′, and ω′=γ(1−9/25)ω=(5/4)(16/25)ω=(4/5)ω=ω/γ, which is less than ω; the axis formulas of [L1] give s1′=(3/5−3/5)/(1−9/25)=0, s2′=(4/5)/[(5/4)(16/25)]=(4/5)/(4/5)=1, s3′=0, so s′=e2.

2.1step 1.1step 1.2∎

Conclusion. In case (a) the shift is by 5/4, in case (b) by 4/5; both configurations are called transverse because the propagation direction is perpendicular to the relative velocity in one of the two frames, and the two factors are different and neither is 1 for the stated nonzero β. Hence a transverse Doppler statement is incomplete until the frame in which transversality holds is specified. The computation is conditional on the ideal plane-wave model and makes no measurement or empirical claim; no choice principle is used.

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Worked aberration and Doppler shift at beta = 3/5 and cos theta = 4/5

Physical scope

Worked numerical aberration and Doppler computation of the ideal plane-wave model at relative speed (3/5)c and source angle cosine 4/5. Conditional on the model; no measurement, statistical inference or empirical claim.

Example

Worked example in the model of sr-light-and-doppler, on the page sr-light-and-doppler-examples. Let x and x′ be inertial charts with x′=B(β)x+b, β=(3/5)e1 and γ=5/4, and let an ideal plane wave have frame-x propagation direction s=(4/5,3/5,0), so cos⁡θ=4/5 and sin⁡θ=3/5 with θ∈[0,π] the angle between s and the boost axis. Then Doppler shift and aberration for an ideal plane wave between inertial descriptions gives s′=(5/13,12/13,0), hence cos⁡θ′=5/13, and the angular frequency ratio ω′/ω=γ(1−βs1)=(5/4)(1−12/25)=(5/4)(13/25)=13/20, so ν′=(13/20)ν and λ′=(20/13)λ. Define the apparent source direction here to mean the incoming unit direction −s (and −s′ in x′); this is a direction convention, not a source or detector model. Since 5/13<4/5 (as 25<52), its axis component moves from −s1=−4/5 to −s1′=−5/13 measured along the boost axis, that is, toward the direction of motion of the observer's frame: this is the sign of stellar aberration in this configuration. The example records the exact direction transformation and leaves any observational interpretation to the framework's experimental work. Scope: a conditional computation in the ideal plane-wave model; no measurement and no empirical claim.

Facts & Assumptions

Given: Inertial charts x,x′ with x′=B(β)x+b, β=(3/5)e1; an ideal plane wave with frame-x direction s=(4/5,3/5,0) and angular frequency ω>0.

[A1]

Wave data and readings: the rest observers of x and x′ read the frequencies ω and ω′, and the linear frequency and wavelength satisfy ν=ω/(2π), λ=c/ν (Null wave covectors, frame frequency data and the observer frequency of an ideal plane wave); the direction and frequency transformation used below is the theorem's (Doppler shift and aberration for an ideal plane wave between inertial descriptions).

[L1]

For the chart pair of the Given the theorem gives ω′=γ(1−β⋅s)ω, and in the axis case β=be1 the direction formulas s1′=(s1−b)/(1−bs1), s2′=s2/[γ(1−bs1)], s3′=s3/[γ(1−bs1)] (Doppler shift and aberration for an ideal plane wave between inertial descriptions, clauses (i) and (ii)).

[L2]

Aberration clause: for β≠0, with θ,θ′ the angles between s,s′ and the boost axis, cos⁡θ′=(cos⁡θ−∣β∣)/(1−∣β∣cos⁡θ) (Doppler shift and aberration for an ideal plane wave between inertial descriptions, clause (v)).

[L3]

γ=(1−∣β∣2)−1/2, so for β=(3/5)e1: γ=(16/25)−1/2=5/4 and ∣β∣=3/5; the boost transformation of the frame data is the one of Boost transformation of a future null wave covector and of its frame data (The passive Lorentz boost with parameter beta).

Verification

technique · direct
1.1A1L1L2L3

The transformed direction. Here s=(4/5,3/5,0) has ∣s∣2=16/25+9/25=1 and s1=4/5; the axis formulas of [L1] with b=3/5 and γ=5/4 [L3] give s1′=(4/5−3/5)/(1−(3/5)(4/5))=(1/5)/(13/25)=5/13, s2′=(3/5)/[(5/4)(13/25)]=(3/5)/(13/20)=12/13 and s3′=0, so s′=(5/13,12/13,0) with ∣s′∣2=25/169+144/169=1; the same value follows from the aberration clause [L2], cos⁡θ′=(4/5−3/5)/(1−(3/5)(4/5))=(1/5)/(13/25)=5/13.

1.2A1L1L3

Frequency and wavelength. By [L1] with β⋅s=(3/5)(4/5)=12/25: ω′/ω=γ(1−12/25)=(5/4)(13/25)=13/20, so ν′=ω′/(2π)=(13/20)ν and λ′=c/ν′=(20/13)λ by [A1].

2.1step 1.1step 1.2L2∎

The apparent direction. By the incoming-direction convention in the Example, the apparent source direction is −s in x and −s′ in x′; its components along the boost axis βhat=e1 are −s1=−4/5 and −s1′=−5/13 by step 1.1. Since 5/13<4/5 (as 25<52), also −5/13>−4/5: the axis component of the apparent direction increases, so the apparent direction moves toward +e1, the direction of motion of the frame x′ relative to x, which is the sign of stellar aberration in this configuration. The computation is conditional on the ideal plane-wave model, records the exact direction transformation, and makes no measurement or empirical claim; no choice principle is used.

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Worked geometry of the phase level sets of a future null wave covector

Example

This worked example computes the geometry of the phase level sets of a future null wave covector. Let (A,V,η,C+) be the oriented time-oriented affine Minkowski space, let k be a future null wave covector with frame data (ϖ,s) in an inertial frame (o;e0,e1,e2,e3) (Frame data of a future null wave covector: the unique pair (ϖ,s) with ∣s∣=1), so that ϖ>0, ∣s∣=1 and k has components ka=(−ϖ,ϖs1,ϖs2,ϖs3) in this frame, and let θ be an affine phase function with wave covector k (Affine phase functions and wave covectors on affine Minkowski space). Then:

(a) k(k♯)=η(k♯,k♯)=0, since the raised vector is k♯=ϖ(e0+s1e1+s2e2+s3e3); hence θ is constant on every line p+Rk♯.

(b) The direction subspace ker⁡k={v:k(v)=0}={v:v0=s⋅vvec} is 3-dimensional; for v∈ker⁡k one has η(v,v)=∣vvec∣2−(s⋅vvec)2≥0 by the finite Cauchy-Schwarz inequality, with equality exactly when vvec is a real multiple of s, that is exactly when v lies in the line span⁡(k♯); hence the restriction of η to ker⁡k is positive semidefinite with radical the line span⁡(k♯), and the only null direction contained in ker⁡k is the line through k♯, with future ray k♯ and past ray −k♯.

(c) Every nonempty level set Σ={p:θ(p)=θ(p0)} is the affine hyperplane p0+ker⁡k through p0, whose normal covector is the null covector k; it contains the two null rays p0+R≥0k♯ and p0+R≤0k♯, and all its other direction vectors are spacelike.

The verification is exact algebra; no choice principle is used.

Facts & Assumptions

Given: An oriented time-oriented affine Minkowski space (A,V,η,C+), a future null wave covector k with frame data (ϖ,s) in an inertial frame (o;e0,e1,e2,e3), and an affine phase function θ with dθ=k.

[L1]

ϖ>0, ∣s∣=1, ka=(−ϖ,ϖs1,ϖs2,ϖs3), k♯=ϖ(e0+s1e1+s2e2+s3e3), and k♯ is nonzero future null with k(k♯)=η(k♯,k♯)=0 (Frame data of a future null wave covector: the unique pair (ϖ,s) with ∣s∣=1, clauses (a)-(d)).

[L2]

k(v)=ϖ(−v0+s1v1+s2v2+s3v3) for every v=v0e0+vvec, and k(v)=0 if and only if θ is constant on every line p+Rv (Affine phase functions and wave covectors on affine Minkowski space, clauses (b)-(c)); ker⁡k is a 3-dimensional linear subspace when k≠0.

[L3]

For the frame, η(v,w)=−v0w0+δ(vvec,wvec) with δ(vvec,wvec)=∑iviwi and ∣vvec∣2=δ(vvec,vvec) (The Euclidean spatial structure and cross product of an inertial frame).

[L4]

Cauchy-Schwarz in root form: ∣∑k<nakbk∣≤∑k<nak2∑k<nbk2, with equality in the squared form exactly when the two lists are proportional in the sense that some (λ,μ)≠(0,0) has λak=μbk for all k; in the frame this gives ∣s⋅vvec∣≤∣s∣ ∣vvec∣ with equality exactly when s and vvec are proportional (The Cauchy-Schwarz inequality for finite sums, The Euclidean inner product ⟨x,y⟩=∑k<nxkyk on Rn).

[L5]

A vector is spacelike when η(v,v)>0, null when nonzero with η(v,v)=0, and the zero vector has no causal character (Timelike, null, spacelike and causal vectors of a Lorentz vector space).

[L6]

k♯ is future null and −k♯ is past null, and every nonzero vector in cl⁡(C+) is future causal (Time orientation, future and past timelike/null/causal vectors, and the closed cones, The timelike set has exactly two convex components, described in orthonormal coordinates).

Verification

technique · direct
1.1L1L2L3

Clause (a). By [L1], k♯=ϖ(e0+∑isiei) with ϖ>0 and ∣s∣=1, so η(k♯,k♯)=ϖ2(−1+∑isi2)=ϖ2(∣s∣2−1)=0 by [L1, L3], and k(k♯)=η(k♯,k♯) by [L1]. For every p∈A and λ∈R the defining identity of the phase gives θ(p+λk♯)=θ(p)+λk(k♯)=θ(p), so θ is constant on the lines p+Rk♯.

2.1step 1.1L2L3L4

Clause (b), kernel and sign. By [L2] and ϖ>0, v∈ker⁡k is equivalent to v0=s⋅vvec, and ker⁡k is a 3-dimensional subspace [L2]. For v∈ker⁡k, substituting v0=s⋅vvec into [L3] gives η(v,v)=−(s⋅vvec)2+∣vvec∣2; by [L4] with ∣s∣=1 this is ≥0, and it is 0 exactly when ∣s⋅vvec∣=∣vvec∣, which by the equality clause of [L4] holds exactly when vvec=λs for some real λ. For such a v, v0=s⋅vvec=λ, so v=λ(e0+∑isiei)=λϖ−1k♯ lies in span⁡(k♯); conversely every multiple of k♯ lies in ker⁡k because k(k♯)=0 by step 1.1. For every w∈ker⁡k one has η(k♯,w)=k(w)=0, so this line lies in the radical; conversely a radical vector has zero self-pairing and thus lies in this line by the equality calculation. Hence η∣ker⁡k is positive semidefinite, its radical is span⁡(k♯), and its only null elements are the nonzero multiples of k♯.

3.1step 2.1L1L5L6

Clause (b), null directions. By [L1] and [L6] the vector k♯ is future null and −k♯ is past null, so the nonzero multiples of k♯ are exactly the two rays R>0k♯ (future null) and R>0(−k♯) (past null) of the line span⁡(k♯); combined with step 2.1 and [L5], the line through k♯ is the only null direction contained in ker⁡k.

4.1step 1.1step 2.1step 3.1L2L5∎

Clause (c). By [L2] and step 2.1 the kernel of the nonzero functional k is the 3-dimensional subspace ker⁡k, and the level set Σ={p:θ(p)=θ(p0)} is the affine hyperplane p0+ker⁡k through p0; its direction subspace is ker⁡k, whose normal covector is k (the linear functional defining the direction subspace), and k is null by hypothesis. Since k♯∈ker⁡k by step 1.1, both rays p0+R≥0k♯ and p0+R≤0k♯ lie in Σ; every other direction vector of Σ lies in ker⁡k outside span⁡(k♯) and is spacelike by steps 2.1 and 3.1 and [L5]. This proves (a), (b) and (c). The computation is exact algebra and no choice principle was used.

CounterexampleConstruction: AI-generatedVerification: AI-generatedOpen item page →

Counterexample: a transverse wave configuration need not have zero Doppler shift

Physical scope

Counterexample to a universal transverse-Doppler claim within the ideal plane-wave model of flat classical special-relativistic spacetime at relative speed (3/5)c. Conditional on the model; no measurement, statistical inference or empirical falsification.

Statement refuted

The following universal claim is refuted: "if the propagation direction of an ideal plane wave is perpendicular to the relative velocity of two inertial frames, then the frequency read by the observer at rest in one frame equals the frequency read by the observer at rest in the other, ω′=ω."

Facts & Assumptions

Given: Inertial charts x and x′ with x′=B(β)x+b, β=(3/5)e1, and an ideal plane wave with frame-x data (ω,s), ω>0, ∣s∣=1, in the ideal plane-wave model.

[A1]

Adopted ideal plane-wave model: the wave is a dimensionless affine phase with future null wave covector, and the rest observers of x and x′ read ω and ω′ as defined in the model (Adopted ideal plane-wave and frequency-reading model, Null wave covectors, frame frequency data and the observer frequency of an ideal plane wave).

[L1]

For the chart pair of the Given, the theorem gives ω′=γ(1−β⋅s)ω>0 with γ=(1−∣β∣2)−1/2, and in the axis case β=be1: s1′=(s1−b)/(1−bs1), s2′=s2/[γ(1−bs1)], s3′=s3/[γ(1−bs1)] (Doppler shift and aberration for an ideal plane wave between inertial descriptions, clause (i)).

[L2]

Transverse protocols of the theorem: if β⋅s=0 then ω′=γω; if β⋅s=∣β∣2, equivalently s′⋅βhat=0 for β≠0, then ω′=ω/γ; in both cases s, s′ are unit and the shift is not one when β≠0 (Doppler shift and aberration for an ideal plane wave between inertial descriptions, clause (iv)).

Counterexample

technique · direct
1.1A1L2algebra

First witness. With β=(3/5)e1 one has ∣β∣2=9/25 and γ=(1−9/25)−1/2=(16/25)−1/2=5/4. Take s=e2; then β⋅s=(3/5)(0)=0, so the propagation direction is perpendicular to the relative velocity in the frame x, and [L2] gives ω′=γω=(5/4)ω≠ω because ω>0. Thus the antecedent of the refuted universal claim holds in x while its conclusion fails.

1.2A1L1L2algebra

Second witness. Take s=(3/5,4/5,0); then ∣s∣2=9/25+16/25=1 and β⋅s=(3/5)(3/5)=9/25=∣β∣2, so by [L2] s′⋅βhat=0, the propagation direction is perpendicular to the relative velocity in the frame x′, and [L2] gives ω′=γ(1−9/25)ω=(5/4)(16/25)ω=(4/5)ω≠ω. Explicitly, the axis formulas of [L1] give s1′=(3/5−3/5)/(1−9/25)=0, s2′=(4/5)/[(5/4)(16/25)]=(4/5)/(4/5)=1 and s3′=0, so s′=e2.

2.1step 1.1step 1.2A1∎

Conclusion. Each witness satisfies the antecedent of the refuted claim — transversality in x in step 1.1 and transversality in x′ in step 1.2 — and yields ω′≠ω; the two factors (5/4) and (4/5) differ and neither equals 1 for the stated nonzero β, so the universal claim is false in the ideal model, and the direction and size of the shift depend on the protocol (the frame in which transversality is required). The counterexample is conditional on the adopted idealizations, performs no measurement and claims no empirical falsification; no choice principle is used.

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Worked frame data of a future null wave covector and its boost

Example

This worked example computes the frame data of a future null wave covector and its passive boost. In an inertial frame (o;e0,e1,e2,e3) let ϖ>0 and s=(0,3/5,4/5), and let k be the covector with frame components (k0,k1,k2,k3)=(−ϖ,0,3ϖ/5,4ϖ/5). Then:

(a) ∣s∣=1 and k is a future null wave covector; its raised vector is k♯=ϖ(e0+(3/5)e2+(4/5)e3) and k(k♯)=0.

(b) Let x′ be the inertial chart with x′=B(β)x+b and β=(3/5)e1. The frame-x′ data of the same covector is (ϖ′,s′) with ϖ′/ϖ=γ(1−β⋅s)=(5/4)(1−0)=5/4 and s′=(−3/5,12/25,16/25).

(c) Applying the transformation with β replaced by −β to (ϖ′,s′) returns (ϖ,s): ϖ′′/ϖ′=(5/4)(16/25)=4/5, so ϖ′′=ϖ, and s′′=(0,3/5,4/5).

The verification is exact rational algebra; no physical interpretation of the data is used, and no choice principle is used.

Facts & Assumptions

Given: An inertial frame (o;e0,e1,e2,e3), a real ϖ>0, s=(0,3/5,4/5), and the covector k with components (k0,k1,k2,k3)=(−ϖ,0,3ϖ/5,4ϖ/5).

[L1]

If a covector has frame components (−ϖ,ϖs1,ϖs2,ϖs3) with ϖ>0 and ∣s∣=1, then it is a future null wave covector; its raised vector is k♯=ϖ(e0+s1e1+s2e2+s3e3) with k(k♯)=η(k♯,k♯)=0 (Frame data of a future null wave covector: the unique pair (ϖ,s) with ∣s∣=1, clauses (d) and (e), The metric pairing is a linear bijection to the dual, and the raised covector in an orthonormal frame).

[L2]

For inertial charts with x′=B(β)x+b, ∣β∣<1, and a future null wave covector with frame-x data (ϖ,s), the frame-x′ data satisfies ϖ′=γ(1−β⋅s)ϖ, si′=[si+γ−1∣β∣2(β⋅s)βi−γβi]/[γ(1−β⋅s)] for β≠0, and in the axis case β=be1: s1′=(s1−b)/(1−bs1), s2′=s2/[γ(1−bs1)], s3′=s3/[γ(1−bs1)]; applying the transformation with −β returns the original data (Boost transformation of a future null wave covector and of its frame data, clauses (ii), (iii), (v)).

[L3]

B(β) is the passive boost of The passive Lorentz boost with parameter beta with γ=(1−∣β∣2)−1/2, and B(β) is proper orthochronous with B(−β)=B(β)−1 (The passive boost is a proper orthochronous Lorentz map with inverse B(-beta)); the frame is an inertial frame with an inertial chart (Inertial frames and inertial charts of the affine Minkowski model).

Verification

technique · direct
1.1L1givenalgebra

Clause (a). Here ϖs=(0,3ϖ/5,4ϖ/5)=(k1,k2,k3) and k0=−ϖ, so the components of k are exactly (−ϖ,ϖs) with ϖ>0; and ∣s∣2=0+(3/5)2+(4/5)2=9/25+16/25=1. By [L1] the covector k is a future null wave covector with k♯=ϖ(e0+(3/5)e2+(4/5)e3), and k(k♯)=η(k♯,k♯)=−ϖ2+ϖ2(0+9/25+16/25)=0.

2.1step 1.1L2L3algebra

Clause (b). With β=(3/5)e1 one has ∣β∣=3/5 and γ=(1−9/25)−1/2=(16/25)−1/2=5/4 [L3, algebra], while β⋅s=(3/5)⋅0+0⋅3/5+0⋅4/5=0. By [L2] the frame-x′ data is ϖ′=γ(1−β⋅s)ϖ=(5/4)(1−0)ϖ=5ϖ/4, and the axis formulas with b=3/5, s1=0, γ=5/4 give s1′=(0−3/5)/(1−0)=−3/5, s2′=(3/5)/((5/4)(1−0))=(3/5)⋅(4/5)=12/25 and s3′=(4/5)⋅(4/5)=16/25. As a check, ∣s′∣2=9/25+144/625+256/625=9/25+16/25=1, in agreement with ∣s′∣=1 in [L2].

3.1step 2.1L2L3algebra∎

Clause (c). Apply [L2] to the chart pair (x′,x), whose transition has parameter −β=−(3/5)e1, and to the data (ϖ′,s′) of step 2.1. Since β⋅s′=(3/5)(−3/5)=−9/25, the factor is γ(1−(−β)⋅s′)=(5/4)(1+β⋅s′)=(5/4)(1−9/25)=(5/4)(16/25)=4/5, so ϖ′′=(4/5)ϖ′=(4/5)(5/4)ϖ=ϖ. The axis formulas with parameter b=−3/5 give s1′′=(s1′−(−3/5))/(1−(−3/5)s1′)=(−3/5+3/5)/(1−9/25)=0, s2′′=s2′/[γ(1−(−3/5)s1′)]=(12/25)/[(5/4)(1−9/25)]=(12/25)/[(5/4)(16/25)]=(12/25)/(4/5)=3/5 and s3′′=(16/25)/(4/5)=4/5. Hence the round trip returns ϖ′′=ϖ and s′′=(0,3/5,4/5), in agreement with clause (v) of [L2]. This proves (a), (b) and (c); all steps are exact rational arithmetic, no physical interpretation of the data was used, and no choice principle was used.

5 · Examples, experiments and counterexamples

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