Positive slow-order tangential stress support #
The moments are actual positive-radius integrals. All radial and parameter operators use the actual Frechet derivatives. Compact stress support is a consequence of the repaired moments and the differential equations.
Actual five-row repair at positive slow order #
Only the order-n entries of the histories are changed. Endpoint extraction proves that all five actual moment increments are linear, including pressure with the known previous-order radial residual retained.
Profile: an abbreviation for ℝ → ℝ.
Equations
Instances For
Cauchy, given by PositiveAxisSystem.convolution n (fun i j => u i R * v j R).
Equations
- NavierStokes.PositiveOrderMoments.cauchy n u v R = NavierStokes.PositiveAxisSystem.convolution n fun (i j : ℕ) => u i R * v j R
Instances For
Increment, given by Function.update u n (fun R => u n R + du R).
Equations
- NavierStokes.PositiveOrderMoments.increment u n du = Function.update u n fun (R : ℝ) => u n R + du R
Instances For
The actual R-pressure equation: Ω is the fixed order-(n-1) source.
Equations
- NavierStokes.PositiveOrderMoments.pressureGradient n e omega R = (NavierStokes.PositiveOrderMoments.cauchy n e e R - omega R) / R
Instances For
The angular similarity coefficient in (22), reconstructed from E.
Equations
- NavierStokes.PositiveOrderMoments.phiHistory C e j R = C * e j R / R
Instances For
Multiplying the actual X-pressure equation by dX/dR=R gives the pressure row used here. In particular the preceding Ω term is retained exactly.
Moments, defined pointwise by positiveIntegral (fun R => rowDensity n u e omega R i).
Equations
- NavierStokes.PositiveOrderMoments.moments n u e omega i = NavierStokes.PositiveOrderMoments.positiveIntegral fun (R : ℝ) => NavierStokes.PositiveOrderMoments.rowDensity n u e omega R i
Instances For
There are no quadratic current-order terms when n>0.
Repair U, given by LocalizedMomentRepair.repair (FiveRowRank.axialPowers lam) (FiveRowRank.cellLower a b) (FiveRowRank.cellUpper a b) (axialDebt A d).
Equations
- One or more equations did not get rendered due to their size.
Instances For
Repair E, constructed using LocalizedMomentRepair.repair.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Exact affine change of all five actual positive-radius integrals.
Arbitrary moment debts are removed, with no size restriction.
Recomputing pressure does not disturb the already solved inner region: the complete new pressure source agrees with the old one up to the patch.
Joint profile: an abbreviation for ℝ × ℝ → ℝ.
Instances For
Slice, defined pointwise by f j (R, eta).
Equations
- NavierStokes.PositiveOrderMoments.slice f eta j R = f j (R, eta)
Instances For
Joint increment, given by Function.update u n (fun w => u n w + du w).
Equations
- NavierStokes.PositiveOrderMoments.jointIncrement u n du = Function.update u n fun (w : ℝ × ℝ) => u n w + du w
Instances For
Global domain, bundling carrier, isOpen, scale_mem.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Compact positive-radius sources identify the actual primitive with the positive-radius total integral, without imposing values at negative radii.
Joint pressure gradient, given by pressureGradient n (slice e w.2) (fun R => omega (R, w.2)) w.1.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Pressure is recomputed from its actual radial gradient, with zero axis datum.
Equations
Instances For
The third repaired row is the actual pressure-exterior condition.
Weighted axial, given by w.1 * u w.
Equations
- NavierStokes.PositiveOrderMoments.weightedAxial u w = w.1 * u w
Instances For
Mass history, given by ProfileHistories.primitive (weightedAxial u).
Equations
Instances For
Parameter mass history, given by ProfileHistories.primitive (ProfileHistories.parameterPartial (weightedAxial u)).
Equations
- One or more equations did not get rendered due to their size.
Instances For
The R-coordinate version of (21), with both histories given by actual integrals.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Radial Z as an element of ℝ.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Genuine radial differentiation of the integral formula gives incompressibility.
The first repaired row is exactly the mass condition making the recomputed radial flux vanish outside the source. Parameter differentiation is justified by the actual smooth history theorem.
The first row of the actual five-moment system gives the required mass condition for the recomputed divergence flux.
The pressure integration-by-parts identity underlying the fifth row is proved for the actual pressure primitive, including its exterior boundary.
Open parameter domains retain all radial histories while keeping the original parameter domain; no extension across its endpoints is needed.
Equations
Instances For
The pressure reconstruction needs smoothness only on the working parameter domain.
The actual radial divergence equation holds on an open parameter domain, without any smooth extension past that domain.
Smoothness of the actual total moment follows from common compact radial support and the proved smooth history theorem.
Joint row density, given by rowDensity n (slice u w.2) (slice e w.2) (fun R => omega (R, w.2)) w.1.
Equations
- One or more equations did not get rendered due to their size.
Instances For
The order-zero angular tail need not be compact: every summand of the positive-order self-convolution contains a strictly positive index.
This statement derives smoothness of the five genuine integral debts; the density hypotheses can be checked componentwise from the known fields.
In particular, the exact zero-moment corrections vary smoothly with η when their debts are the actual profile integrals, not prescribed surrogates.
The integrability requirements of the repair theorem follow from the same common compact support and smoothness used for the parameter jets.
A single explicit smooth family repairs all five rows on the parameter domain. Its debts are the actual finite-profile integrals; only order n is changed, and the known Ω term remains untouched.
Field: an abbreviation for ℝ × ℝ → ℝ.
Instances For
Dr, given by ProfileHistories.radialPartial.
Instances For
De, given by ProfileHistories.parameterPartial.
Instances For
Axial Op2, given by axialOp h (b - PositiveAxisSystem.dScale h) (axialOp h b f).
Equations
Instances For
Order exponent, given by -PositiveAxisSystem.a h + SlowExpansionResidual.slowOrder h n.
Equations
Instances For
Pressure exponent, given by -2 * PositiveAxisSystem.a h + SlowExpansionResidual.slowOrder h n.
Equations
Instances For
At a fixed convolution order the physical power is independent of the split.
Conv, given by ∑ i ∈ Finset.range (n + 1), u i w * v (n - i) w.
Equations
- NavierStokes.SlowStressSupport.conv n u v w = ∑ i ∈ Finset.range (n + 1), u i w * v (n - i) w
Instances For
Angular viscous flux, given by w.1 ^ 2 * dr e w - w.1 * e w.
Equations
- NavierStokes.SlowStressSupport.angularViscousFlux e w = w.1 ^ 2 * NavierStokes.SlowStressSupport.dr e w - w.1 * e w
Instances For
Incompressibility converts the actual angular advection terms to conservative form; the convolution exponents are checked, not assumed.
The integrated angular equation, with the previous axial-viscosity term still displayed. The other four terms cancel by the repaired moments and the actual radial boundary terms.
Pressure integration by parts turns the fifth repaired row into the zero total axial momentum flux. The pressure derivative is an actual one.
All moment hypotheses used in the integrated balances follow from the five repaired rows. Pressure is the actual forward primitive of its source.
The negative weighted radial primitive. The definition is zero on nonpositive radii; vanishing of the source near the axis makes this smooth.
Equations
- NavierStokes.SlowStressSupport.stress m F w = if 0 < w.1 then -NavierStokes.ProfileHistories.primitive F w / w.1 ^ m else 0
Instances For
Every actual derivative tensor has a weighted bound because its support lies in one fixed compact subinterval of the positive-weight region. No stress norm bound is an input. The constant may depend on the derivative order.
A fixed interior support interval gives all weighted stress jets on every compact parameter subinterval, as well as a smooth normalized stress.
Angular stress, given by stress 2 (angularDensity h n v u e).
Equations
Instances For
For n≥2 all the angular hypotheses below are supplied by ordinary positive-order moments and compact positive-order profiles.
The order-one angular input is a moment of the actual axial viscosity, not a condition on the total residual. It is supplied by differentiating the restored renormalized order-zero physical angular moment.
Equations
- One or more equations did not get rendered due to their size.
Instances For
A concrete two-edge weight of the form prescribed in (20).
Equations
- One or more equations did not get rendered due to their size.
Instances For
In particular the prescribed logarithmic Gaussian weight controls every jet, with inverse-edge loss zero, for a field supported strictly inside both fixed edges. The constants are obtained from compactness.