The physical heat edit: diffusion is 1 - eta^2 #
The diffusion variable is allowed to reach zero. All endpoint derivatives below are derivatives within the closed parameter domain; no extension to negative diffusion is assumed.
Differentiation of dominated derivative chains on the closed half-line #
The domination is uniform in the parameter on each bounded interval.
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Explicit algebra of genuine derivative chains #
Recursive Leibniz product. Its derivative identity is proved below.
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- NavierStokes.ParametricHeatTail.jetProduct a b 0 = a 0 * b 0
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The actual diffusion jets of the switched multiplier #
Heat jet bound, given by |(Real.Gamma (1 + h))⁻¹ * RadialHeatProfile.derivativeCoeff (1 + h) n| * Real.Gamma (1 + h + (n : ℝ)).
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- NavierStokes.ParametricHeatTail.heatJetBound h n = |(Real.Gamma (1 + h))⁻¹ * NavierStokes.RadialHeatProfile.derivativeCoeff (1 + h) n| * Real.Gamma (1 + h + ↑n)
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Correction jet used in parametric heat tail.
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- NavierStokes.ParametricHeatTail.correctionJet h K 0 x✝¹ x✝ = NavierStokes.HeatTailEdit.switch K x✝ * (NavierStokes.RadialHeatProfile.profile (1 + h) (2 * x✝¹ / x✝) - 1)
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Correction bound as an element of ℕ → ℝ | 0 => heatConstant h L | n + 1 => 2 ^ (n + 1) * heatJetBound h (n + 1).
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Square correction bound, given by 2 * correctionBound h L n + jetProduct (correctionBound h L) (correctionBound h L) n.
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Actual improper integrals of the diffusion jets #
Weighted jet, given by X ^ q * W X * editJet square h K n ν X.
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- NavierStokes.ParametricHeatTail.weightedJet W square h K q n ν X = X ^ q * W X * NavierStokes.ParametricHeatTail.editJet square h K n ν X
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Weighted debt jet, given by ∫ X in Ioi K, weightedJet W square h K q n ν X.
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- NavierStokes.ParametricHeatTail.weightedDebtJet W square h K q n ν = ∫ (X : ℝ) in Set.Ioi K, NavierStokes.ParametricHeatTail.weightedJet W square h K q n ν X
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The actual outgoing shape and the three physical debts #
Tail weight, with branches according to square.
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Tail decay, with branches according to square.
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- NavierStokes.ParametricHeatTail.tailDecay d square = if square = true then -2 * NavierStokes.HeatTailEdit.exponent d.h else -NavierStokes.HeatTailEdit.exponent d.h
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Tail size, with branches according to square.
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Nu debt jet, given by weightedDebtJet (tailWeight d K square) square d.h K q n ν.
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- NavierStokes.ParametricHeatTail.nuDebtJet d K square q n ν = NavierStokes.ParametricHeatTail.weightedDebtJet (NavierStokes.ParametricHeatTail.tailWeight d K square) square d.h K q n ν
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Nu constant, given by tailSize d square * editBound square d.h 1 n / (-tailDecay d square - q).
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Diffusion, given by 1 - eta ^ 2.
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- NavierStokes.ParametricHeatTail.diffusion eta = 1 - eta ^ 2
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Physical pressure, given by pressureDebt (outgoingProfile d K eta) d.h (diffusion eta) K.
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Physical energy, given by energyDebt (outgoingProfile d K eta) d.h (diffusion eta) K.
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Physical angular, given by angularDebt (outgoingProfile d K eta) d.h (diffusion eta) K.
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Composition with the physical diffusion 1 - eta^2 #
Eta debt, given by nuDebtJet d K square q 0 (diffusion eta).
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- NavierStokes.ParametricHeatTail.etaDebt d K square q eta = NavierStokes.ParametricHeatTail.nuDebtJet d K square q 0 (NavierStokes.ParametricHeatTail.diffusion eta)
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Eta constant, given by (n.factorial : ℝ) * (∑ i ∈ Finset.range (n + 1), nuConstant d square q i) * 2 ^ n.
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- NavierStokes.ParametricHeatTail.etaConstant d square q n = (↑n.factorial * ∑ i ∈ Finset.range (n + 1), NavierStokes.ParametricHeatTail.nuConstant d square q i) * 2 ^ n
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Every fixed genuine eta jet has the manuscript's three unnormalized scales.
A single constant controls values and actual first within derivatives. This is the scalar input to the variable-debt nonlinear compensation theorem.
Endpoint jets and the velocity in physical units #
Physical edit, given by outgoingEdit d (diffusion eta) K eta X.
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The similarity prefactor cancels all powers of q. The carrier is
exactly a constant times s^(-A) H(2 tau / s).
The eta derivatives are not identically zero. In particular, the actual
one-sided angular derivative at the physical endpoint eta = 1 is positive.