The explicit shape transition and its reset-prefix debts #
The cutoff and target shape are the actual functions from OutgoingSchedule.
Input field bounds are pointwise bounds, not assumptions on the five row debts.
All constants in the estimates may be chosen before the final large C.
Log profile, given by -Real.log C + p.1 / 10 + blend T li p.
Equations
- NavierStokes.ShapeTransition.logProfile C T li p = -Real.log C + p.1 / 10 + NavierStokes.ShapeTransition.blend T li p
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Angular, given by Real.exp (logProfile C T li p).
Equations
- NavierStokes.ShapeTransition.angular C T li p = Real.exp (NavierStokes.ShapeTransition.logProfile C T li p)
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Smoothness above and exact equalities on both closed half-lines give the actual smooth gluing. The following statement records all radial jets on the open constant-profile regions as well.
A duration chosen before C #
Logarithmic slope, given by 3 / 5 + deriv OutgoingSchedule.sigma (p.1 / T) / T * (logShape p.2 - li p.2).
Equations
- NavierStokes.ShapeTransition.logarithmicSlope T li p = 3 / 5 + deriv NavierStokes.OutgoingSchedule.sigma (p.1 / T) / T * (NavierStokes.ShapeTransition.logShape p.2 - li p.2)
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Uniform finite parameter jets from the input jets #
The reset clock and exact ideal matching #
Reset radius, given by Xi * (C * P) ^ 10.
Equations
- NavierStokes.ShapeTransition.resetRadius Xi C P = Xi * (C * P) ^ 10
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Ideal angular, given by P * OutgoingSchedule.shape p.2 * Real.exp (p.1 / 10).
Equations
- NavierStokes.ShapeTransition.idealAngular P p = P * NavierStokes.OutgoingSchedule.shape p.2 * Real.exp (p.1 / 10)
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Actual restoration on reset-clock times -8 to -7 #
Restore, given by (1 - OutgoingSchedule.sigma (p.1 + 8)) * Gi p.2 + OutgoingSchedule.sigma (p.1 + 8) * (4 * p.2).
Equations
- NavierStokes.ShapeTransition.restore Gi p = (1 - NavierStokes.OutgoingSchedule.sigma (p.1 + 8)) * Gi p.2 + NavierStokes.OutgoingSchedule.sigma (p.1 + 8) * (4 * p.2)
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A smooth physical-radius implementation, including the old axis piece #
The harmless zero extension avoids evaluating the logarithmic clock at the axis. On every positive radius this is exactly the cutoff in (19).
Equations
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The supplied old normalized field is continued by its held power law past
Xi. Multiplication by this explicit smooth factor performs the transition.
Equations
- NavierStokes.ShapeTransition.shapeField Xi T li old p = old p * Real.exp (NavierStokes.ShapeTransition.radialSwitch Xi T p.1 * (NavierStokes.ShapeTransition.logShape p.2 - li p.2))
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Actual compact integrals and their parameter jets #
The five actual scaled history rows #
All five finite-jet estimates are estimates of the actual row integrals. Only the parameter jets of the two input fields are bounded in the hypotheses.
The following coefficient contains only fixed upstream data.
Uniformity in the external parameter is obtained from uniform input-jet
bounds. The fixed duration, data bounds, and physical prefix length precede C.
The ideal prefix has small rows too #
Ideal M, given by r * G eta.
Equations
- NavierStokes.ShapeTransition.idealM G r eta = r * G eta
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Ideal J, given by idealWeightI r * (G eta * A eta).
Equations
- NavierStokes.ShapeTransition.idealJ G A r eta = NavierStokes.ShapeTransition.idealWeightI r * (G eta * A eta)
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Ideal S, given by r * G eta ^ 2 - idealWeightS r * A eta ^ 2.
Equations
- NavierStokes.ShapeTransition.idealS G A r eta = r * G eta ^ 2 - NavierStokes.ShapeTransition.idealWeightS r * A eta ^ 2
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Ideal P, given by idealWeightP r * A eta ^ 2.
Equations
- NavierStokes.ShapeTransition.idealP A r eta = NavierStokes.ShapeTransition.idealWeightP r * A eta ^ 2
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Ideal prefix coefficient, given by `B + 2 * K + 2 * (2 ^ n * B * K) + 2 ^ n * B ^ 2 + (2 ^ n
- K ^ 2) / 2`.
Equations
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Genuine restoration debts on a positive compact interval #
Restore defect, given by restore Gi (Real.log p.1, p.2) - 4 * p.2.
Equations
- NavierStokes.ShapeTransition.restoreDefect Gi p = NavierStokes.ShapeTransition.restore Gi (Real.log p.1, p.2) - 4 * p.2
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Restore density J, given by (Real.sqrt (2 * p.1) * p.1 ^ (1 / 10 : ℝ)) * (restoreDefect Gi p * A p.2).
Equations
- NavierStokes.ShapeTransition.restoreDensityJ Gi A p = √(2 * p.1) * p.1 ^ (1 / 10) * (NavierStokes.ShapeTransition.restoreDefect Gi p * A p.2)
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Restore density S, given by restoreDefect Gi p * (restore Gi (Real.log p.1, p.2) + 4 * p.2).
Equations
- NavierStokes.ShapeTransition.restoreDensityS Gi p = NavierStokes.ShapeTransition.restoreDefect Gi p * (NavierStokes.ShapeTransition.restore Gi (Real.log p.1, p.2) + 4 * p.2)
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The angular field is unchanged during restoration; its two pure-angular rows have zero restoration debt. These are the other three actual row debts.
Subtracting the ideal rows and including restoration #
Reset debt I, given by rowI R f r eta - idealI A r eta.
Equations
- NavierStokes.ShapeTransition.resetDebtI R f A r eta = NavierStokes.ShapeTransition.rowI R f r eta - NavierStokes.ShapeTransition.idealI A r eta
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Reset debt P, given by rowP R f r eta - idealP A r eta.
Equations
- NavierStokes.ShapeTransition.resetDebtP R f A r eta = NavierStokes.ShapeTransition.rowP R f r eta - NavierStokes.ShapeTransition.idealP A r eta
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Vanishing debt bound as an element of ℝ.
Equations
- One or more equations did not get rendered due to their size.
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Restoration bound, given by delta * (1 + 2 * (2 ^ n * KA) + 2 ^ n * (delta + 2 * BG)).
Equations
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Increasing C removes only the prefix term. The explicit restoration term
is retained, so the upstream smallness choice is not silently changed.
Direct adapter from axis and entry jets to the constructed prefix #
This theorem assumes axis-field jets and the held entry power law, then
derives the actual constructed prefix-row estimates. No row-smallness
hypothesis occurs. The constant shapeJetConstant is independent of C.
The row-debt decomposition used above is the ordinary split of actual integrals at the separation radius.