Actual outgoing histories through the axial drop #
All lags below include the ideal incoming history. The scalar averages are integrals of the constructed schedule, and no cone estimate is assumed.
Exponential averaging with the actual incoming history at clock zero.
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- NavierStokes.OutgoingEntranceCone.historyAverage b b₀ y = NavierStokes.OutgoingTail.linearLag (fun (x : ℝ) => 1) b b₀ y
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The actual average axial coefficient; the incoming value integrates k=4.
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The squared axial history; the incoming value integrates k²=16.
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Shape gradient, given by 2 * η / (1 + η ^ 2).
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Drop speed, given by 4 * stepBound / m.
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The actual angular source and its ideal incoming lag #
Transport W, given by 1 - L h η * averagedDrop c y.
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Angular rate, given by 1 + slope c.dropLength c.lam y.
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Angular source as an element of ℝ.
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Ideal angular source, given by (3 / 5) * (4 * L h η - 1) - h * (1 - 8 * η ^ 2) + (D h + 4 * d η) * η * shapeGradient η.
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Angular lag, given by linearLag (angularRate c) (angularSource c h η) (idealAngularLag h η).
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The positive angular lag is derived from its incoming ideal integral and
the true source. The constant is absolute and uniform in P, λ, h, m.
The actual angular-energy history #
Clock energy, given by radialAmplitude c.P c.dropLength c.lam y ^ 2.
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Weighted clock energy, given by Real.exp y * clockEnergy c y.
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Averaged clock energy, given by historyAverage (clockEnergy c) ((5 / 6) * c.P ^ 2).
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Averaged energy, given by shape η ^ 2 * averagedClockEnergy c y.
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Pressure and the axial lag with the full ideal incoming history #
Pressure clock, given by (5 / 2) * c.P ^ 2 + (1 / 2) * OutgoingSchedule.primitive (clockEnergy c) y.
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Entrance pressure, given by SchedulePressure.axisPressure v η + shape η ^ 2 * pressureClock v.core y.
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Pressure gradient, given by `deriv (SchedulePressure.axisPressure v) η - 2 * shapeGradient η
- shape η ^ 2 * pressureClock v.core y`.
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The part of the axial lag arising from the actual mass and squared-axial histories.
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The pressure and angular-energy part of the integrated axial lag.
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Axial lag, given by geometricAxialLag v.core v.h y η + pressureAxialLag v y η.
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Geometric axial source as an element of ℝ.
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Pressure axial source as an element of ℝ.
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Axial source, given by geometricAxialSource v.core v.h y η + pressureAxialSource v y η.
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Normalized energy history S/X, including both ideal-prefix integrals.
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This is precisely the axial integrated-history formula (9); the linear
mass-history contribution D(M-η Mη)/X vanishes for U=k(y)η.
Pressure bound, given by 10 * FuturePressureBounds.envelopeConstant.
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The actual full axial lag has the required normalized drop bound. The geometric part is suppressed by choosing the fixed prefix amplitude first.
The two small shear quantities in the cone test #
Shear, given by 2 * deriv (dropCoefficient c.m) y * η / angular c.P c.dropLength c.lam (y, η).
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- NavierStokes.OutgoingEntranceCone.shear c y η = 2 * deriv (NavierStokes.OutgoingSchedule.dropCoefficient c.m) y * η / NavierStokes.OutgoingSchedule.angular c.P c.dropLength c.lam (y, η)
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Direction ratio, given by axialLag v y η / (angular v.core.P v.core.dropLength v.core.lam (y, η) * angularLag v.core v.h η y).
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Radial A, given by 2 - 2 * slope c.dropLength c.lam y.
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Quantified strict margins in the preliminary drop cone.
A parameter-uniform bound at the shaped-wait entrance #
Entrance ratio bound as an element of ℝ.
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A fixed pre-λ bound on the ratio throughout the first ramp, drop, and
shaped-wait entrance. It depends only on the already fixed P,m.
Identification with the canonical, incoming-history fields #
The positive scalar lag is exactly the canonical integrated angular stress. No positivity or cone assumption is used in this identification.
The first and last preliminary ramps #
Uniform pressure-source estimates #
A single ordered choice of the preliminary parameters #
Drop threshold, given by min (1 / 8) (coneFloor / (16 * axialBound)).
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Lambda threshold, given by min (1 / 20) (1 / (4 * (entranceRatioBound P m ^ 2 + 1))).
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- NavierStokes.OutgoingEntranceCone.lambdaThreshold P m = min (1 / 20) (1 / (4 * (NavierStokes.OutgoingEntranceCone.entranceRatioBound P m ^ 2 + 1)))
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Height threshold, given by min (1 / 100) (min (lam / 4) (Real.exp (-(entranceTime m + 3 / 5)) / 8)).
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- NavierStokes.OutgoingEntranceCone.heightThreshold m lam = min (1 / 100) (min (lam / 4) (Real.exp (-(NavierStokes.OutgoingEntranceCone.entranceTime m + 3 / 5)) / 8))
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The drop is chosen first. All subsequent cutoffs display precisely which earlier parameters they depend on; the cone constants are absolute.
The actual stress-cone fields and finite amplitude #
Cone A, given by 2 - 2 * (OutgoingHistories.dY (OutgoingHistories.H w) p / OutgoingHistories.H w p).
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Cone B, given by 2 * OutgoingHistories.dY (OutgoingHistories.U v Amp) p / OutgoingHistories.E w p.
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Cone ratio, given by OutgoingHistories.Ns w Amp p / (OutgoingHistories.E w p * OutgoingHistories.Qs w Amp p).
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- NavierStokes.OutgoingEntranceCone.coneRatio w Amp p = NavierStokes.OutgoingHistories.Ns w Amp p / (NavierStokes.OutgoingHistories.E w p * NavierStokes.OutgoingHistories.Qs w Amp p)
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Preliminary window, given by Icc 0 v.core.holdStart ×ˢ Icc (-1) 1.
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Uniform finite-amplitude relaxed cone for the actual history stresses on the whole preliminary interval. Both root inequalities have a common gap.
A single large physical radial scale gives the actual relaxed cone, uniformly in the complete first-ramp/drop/entrance region.
The same canonical identification is valid to the left of clock zero.
The radial normal coefficient agrees with the logarithmic derivative of
the true angular field E, rather than a declared slope proxy.
Ordered parameter selection for actual histories, followed by the final
physical radial-scale choice. All thresholds before XR are explicit.