claimroutine
Radial solutions dominate log-affine interpolants
Radial solutions of dominate log-affine interpolants
comparison function for outward and return passages
Statement (paper)
Let and be fixed, and let solve on with endpoint values in either order. Then is bounded below by a constant (depending on , ) times the function affine in with the same endpoint values; in the notation , , the solution of with , satisfies on , and the same bound holds for the reversed ordering of boundary values.
In plain English
For the radial equation on with and boundary values and in either order, the solution is at least a constant (depending on ) times the interpolant that is affine in . In the variable this says on , where , , , , and likewise for the reversed boundary values.
Why it's here
This gives a quantitative lower bound for radial solutions across the thin cylinder, with the loss only a constant multiple of the log-linear profile and no extra powers of . The later claims use it as a comparison function to bound the band mass from below on the outward passage and on the return passage to inner radius , which produces the factor in the lemma.
Classified routine:
A standard ODE comparison argument: after the substitution the radial equation becomes with , and convexity/Sturm comparison bounds the solution below by a constant times the linear interpolant. It is a technical step inside the cylinder lemma, not a new idea.
Uses
Nothing else in the paper
Used by
Figures
Figure 2schematicp. 22
The two comparisons, with radii drawn schematically. The boundary mass on bounds the mass in the shaded band from below. The mean inequality on a fixed annulus supplies a lower bound on the entire upper wall in (b). The two displayed fractions are values of the normalized radial harmonic functions. The comparison solutions with potential dominate fixed multiples of these values, giving the factor at the dot. In the wave estimate, : controls the wave norm on the marked segment and is controlled by the initial data at the dot.
What it shows
Two side-by-side rectangles in the plane, with drawn schematically. Panel (a), "Outward comparison", spans and . A thick orange segment labelled "observed wave" lies on the bottom wall for , and a shaded band is centred on a dashed line at ; below it is the factor at , . Panel (b), "Inward comparison", spans and . Its thick teal top wall at is labelled "uniform lower bound", and dashed guides mark an orange dot at labelled ; below it is the factor at , . Together the panels show the two logarithmic losses incurred in carrying the energy out to and back to the inner wall.
Read from the image by claude-opus-5.5 · confidence 88%
Sources
PaperOpen
- Section
- §6 Propagation across a thin cylinder
- Page
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- Label
—- Line
sections/propagation.tex:38
Leannot aligned
Phase 2 aligns this node to a Lean declaration.