Changes of the literal mean equations under an actual mean increment #
The differential operators below are genuine graph derivatives. The nonlinear fields are the products in equation (32), including every old/new mean cross term. The unchanged wave covariance and virtual flux cancel only after an exact residual-difference identity.
Field: an abbreviation for ℕ → D → ℝ.
Equations
- NavierStokes.MeanIncrementBounds.Field D = (ℕ → D → ℝ)
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Operators data, collecting epsilon, radialFrequency, fastCoefficient, radius,
radialProfile, eR and their compatibility conditions.
The smallness parameter at each stage.
Radial frequency of
Operators, of typeℕ → ℝ.Fast coefficient of
Operators, of typeℕ → ℝ.- radius : D → ℝ
- radialProfile : D → ℝ
- eR : D
- eZ : D
- eT : D
- vR : D
- vT : D
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Dr, given by graphDerivative o.radialFrequency o.radialProfile o.eR o.vR f.
Equations
- o.dr f = NavierStokes.WeightedClasses.graphDerivative o.radialFrequency o.radialProfile o.eR o.vR f
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Slow time, defined pointwise by -(o.epsilon n * fderiv ℝ (f n) x o.eT).
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Fast time, defined pointwise by o.fastCoefficient n * fderiv ℝ (f n) x o.vT.
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The connection parameter is one for radial/angular velocity, zero axially.
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Smooth on, given by ∀ n, ContDiffOn ℝ ∞ (f n) U.
Equations
- NavierStokes.MeanIncrementBounds.SmoothOn U f = ∀ (n : ℕ), ContDiffOn ℝ (↑⊤) (f n) U
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Agree, given by ∀ n, EqOn (f n) (g n) U.
Equations
- NavierStokes.MeanIncrementBounds.Agree U f g = ∀ (n : ℕ), Set.EqOn (f n) (g n) U
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Operator bounds data, collecting epsilon_eq, radialProfile, invRadius,
radialFrequency, fastCoefficient, kappa_nonneg and their compatibility conditions.
- radialProfile : WeightedClasses.UnweightedClass s 0 fun (x : ℕ) => o.radialProfile
- invRadius : WeightedClasses.UnweightedClass s 0 o.invRadius
- radialFrequency : WeightedClasses.BandBound s (-κ) o.radialFrequency
- fastCoefficient : WeightedClasses.BandBound s 0 o.fastCoefficient
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Theta residual, constructed using o.time.
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- One or more equations did not get rendered due to their size.
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Axial residual, constructed using o.time.
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- One or more equations did not get rendered due to their size.
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- One or more equations did not get rendered due to their size.
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Delta theta axial, given by `b.axial * h.angular + b.angular * h.axial + m.axial * h.angular
- h.axial * m.angular + h.axial * h.angular`.
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Radial remainder as an element of Field D.
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- One or more equations did not get rendered due to their size.
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Theta remainder, given by o.slowTime h.angular + o.radialDiv 2 (deltaThetaRadial b m h) + o.dz (deltaThetaAxial b m h) - o.viscosity 1 h.angular.
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- One or more equations did not get rendered due to their size.
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Axial remainder, given by o.slowTime h.axial + o.radialDiv 1 (deltaAxialRadial b m h) + o.dz (deltaAxialAxial b m h + δp) - o.viscosity 0 h.axial.
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- One or more equations did not get rendered due to their size.
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Base bounds data, collecting radial, angular, axial.
- radial : WeightedClasses.UnweightedClass s 1 b.radial
- angular : WeightedClasses.UnweightedClass s 0 b.angular
- axial : WeightedClasses.UnweightedClass s 0 b.axial
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Cumulative bounds data, collecting radial, angular, axial.
- radial : WeightedClasses.MeanClass s (19 / 10) m.radial
- angular : WeightedClasses.MeanClass s (9 / 10) m.angular
- axial : WeightedClasses.MeanClass s (9 / 10) m.axial
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Increment bounds data, collecting radial, angular, axial.
- radial : WeightedClasses.MeanClass s (H + 1) h.radial
- angular : WeightedClasses.MeanClass s H h.angular
- axial : WeightedClasses.MeanClass s H h.axial
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Every non-leading term of the actual radial pressure-source change has the stronger defect exponent. This includes fast time on the radial stream.
The actual radial source change retains the leading centrifugal term.
Independence along an actual affine line removes its Fréchet derivative.
A field depending only on the slow projection has no fast derivative.
An interior radial cutoff belongs to the same flat mean class. The constant comes from its actual jets and the positive weight on its support.
The density in (33) is the actual normalized bump, not an assumed flat multiplier.
Recomputing (33) after an update is exactly applying its linear integral operator to the actual radial source difference.
The actual normalized shifted pressure primitive preserves every fixed-jet mean class, uniformly over its radial and torus shifts.
Reconstructed pressure, defined pointwise by PressureStream.meanPressure d a b (M n) hab (v n) (gr o base mean W n).
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- One or more equations did not get rendered due to their size.
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Pressure is recomputed from the literal gr; its change class is a
conclusion, obtained from the centrifugal term and the exact remainder.
Every tangential effect beyond the actual fast derivative has the claimed exponent, including the recomputed axial pressure contribution.
In the slow rank update the fast derivatives vanish, so the estimates hold directly for the full changes of the tangential residuals.
The physical-coordinate instance identifies the chart expressions above
with the already formalized equation (32). The slow time direction is -∂t
because the chart's slow time term has a minus sign.
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- One or more equations did not get rendered due to their size.
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Physical field, defined pointwise by f.
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Physical triple, given by ⟨physicalField (b 0), physicalField (b 1), physicalField (b 2)⟩.
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- One or more equations did not get rendered due to their size.
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Physical covariance, defined pointwise by physicalField (MeanResidual.covariance w i j).