Actual history limits on the pure heat tail #
All tail integrals below are actual improper integrals. Their differentiated kernels have explicit integrable power majorants. The physical histories use the same outgoing profile and the same compensation witness throughout.
Differentiated heat corrections and their actual tail integrals #
Tail kernel, given by u ^ (-k) * ExtendedHeatDebts.editJet square h 1 n ν u.
Equations
- NavierStokes.HeatTailHistoryLimits.tailKernel square h k n ν u = u ^ (-k) * NavierStokes.ExtendedHeatDebts.editJet square h 1 n ν u
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Tail jet, given by ∫ u in Ioi X, tailKernel square h k n ν u.
Equations
- NavierStokes.HeatTailHistoryLimits.tailJet square h k n X ν = ∫ (u : ℝ) in Set.Ioi X, NavierStokes.HeatTailHistoryLimits.tailKernel square h k n ν u
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Eta tail, given by tailJet square h k 0 X (ParametricHeatTail.diffusion η).
Equations
- NavierStokes.HeatTailHistoryLimits.etaTail square h k X η = NavierStokes.HeatTailHistoryLimits.tailJet square h k 0 X (NavierStokes.ParametricHeatTail.diffusion η)
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Exact exterior formulas for the supplied outgoing profile #
Amplitude, given by RenormalizedHeatMoment.outgoingPowerAmplitude F XR.
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Angular amplitude, given by Real.sqrt 2 * amplitude F XR.
Equations
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Tail start, given by max (RenormalizedHeatMoment.heatThreshold F XR) (Real.exp 1).
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The constants are fixed by the same compensation witness #
Angular history, given by ∫ u in Ioc 0 X, HeatedOutgoing.H F XR c (u,η).
Equations
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Energy history, given by ∫ u in Ioc 0 X, HeatedOutgoing.energyDensity F XR c η u.
Equations
- NavierStokes.HeatTailHistoryLimits.energyHistory F XR c η X = ∫ (u : ℝ) in Set.Ioc 0 X, NavierStokes.HeatedOutgoing.energyDensity F XR c η u
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Power history, given by ∫ u in Ioc 0 X, OutgoingDilation.powerH F XR u.
Equations
- NavierStokes.HeatTailHistoryLimits.powerHistory F XR X = ∫ (u : ℝ) in Set.Ioc 0 X, NavierStokes.OutgoingDilation.powerH F XR u
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Genuine parameter derivatives and the history limits #
The actual angular field and its radial derivative at infinity #
Heat H, given by D * X ^ (-h) * heatFactor h η X.
Equations
- NavierStokes.HeatTailHistoryLimits.heatH h D η X = D * X ^ (-h) * NavierStokes.HeatTailHistoryLimits.heatFactor h η X
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Factor slope, given by -h * heatFactor h η X - (2 * (1 - η ^ 2) / X) * deriv (HeatProfileExtension.extension (1 + h)) (2 * (1 - η ^ 2) / X).
Equations
- One or more equations did not get rendered due to their size.
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All required history limits for one and the same actual heat completion.