The stock-driven ACT continuation and its final two ramps #
The controls below integrate the actual reference lag stocks. The axial
control is turned off first; the angular control is then interpolated to
4 / 5. All profile values are defined by integrals, including at the
joins. No cone inequality is assumed here.
A translated copy of the manuscript's flat step.
Equations
- NavierStokes.TransitionRamp.step b w y = NavierStokes.OutgoingSchedule.sigma ((y - b) / w)
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A literal primitive, with an independently specified value at the axis of the logarithmic clock.
Equations
- NavierStokes.TransitionRamp.integrate initial slope p = initial p.2 + NavierStokes.ProfileHistories.primitive slope p
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The ordinary ACT control continues to multiply the REF lag stock, even when the REF derivative has already become zero.
Equations
- NavierStokes.TransitionRamp.baseSlope T κ stock p = -(NavierStokes.StressActivation.damping T κ p.1 * stock p) / 2
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Angular slope, defined pointwise by (1 - step (b + w₁) w₂ p.1) * baseSlope T κ stock p - (2 / 5 : ℝ) * step (b + w₁) w₂ p.1.
Equations
- One or more equations did not get rendered due to their size.
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Axial slope, defined pointwise by (1 - step b w₁ p.1) * baseSlope T κ stock p.
Equations
- NavierStokes.TransitionRamp.axialSlope T κ b w₁ stock p = (1 - NavierStokes.TransitionRamp.step b w₁ p.1) * NavierStokes.TransitionRamp.baseSlope T κ stock p
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The actual logarithm of the angular amplitude.
Equations
- NavierStokes.TransitionRamp.logField T κ b w₁ w₂ initial stock = NavierStokes.TransitionRamp.integrate initial (NavierStokes.TransitionRamp.angularSlope T κ b w₁ w₂ stock)
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The actual axial velocity after the first, axial, shutoff.
Equations
- NavierStokes.TransitionRamp.axialField T κ b w₁ initial stock = NavierStokes.TransitionRamp.integrate initial (NavierStokes.TransitionRamp.axialSlope T κ b w₁ stock)
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Genuine reference profiles, with their positive-radius logarithmic chart. The two controls below are defined from their actual lag integrals.
- exponent : ℝ
Exponent of
StockReference, of typeℝ. - radius0 : ℝ
Radius0 of
StockReference, of typeℝ. - domain : ProfileHistories.RadialDomain
Domain of
StockReference, of typeRadialDomain. - profiles : ProfileHistories.Profiles self.domain
Profiles of
StockReference, of typeProfiles domain. - L_ne_zero (η : ℝ) : η ∈ J → NaturalAxisData.L self.exponent η ≠ 0
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Chart, given by (radius R.radius0 p.1, p.2).
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Angular stock, defined pointwise by ActivationStocks.profileStockOne R.profiles R.exponent (R.chart p).
Equations
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This is X * ns_REF, including the radial factor in the axial ODE.
Equations
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Log amplitude, given by logField T κ R.bigTime w₁ w₂ R.initialLog R.angularStock.
Equations
- R.logAmplitude T κ w₁ w₂ = NavierStokes.TransitionRamp.logField T κ R.bigTime w₁ w₂ R.initialLog R.angularStock
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Axial velocity, given by axialField T κ R.bigTime w₁ R.initialU R.axialStock.
Equations
- R.axialVelocity T κ w₁ = NavierStokes.TransitionRamp.axialField T κ R.bigTime w₁ R.initialU R.axialStock
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Actual parameter jets of the integral controls #
Parameter jet as an element of ℕ → Field → Field | 0, F => F | n + 1, F => parameterPartial (parameterJet n F).
Equations
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A modification supported after a contributes only the traversed
width; the estimate applies before, during, and at the end of its ramp.
Integrating the actual damping gives a bound proportional to the activation width plus the retained constant control.
Instantiation by the constructed natural profiles #
Log point, given by (R.logTime p.1, p.2).
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Physical F, defined pointwise by if p.1 ≤ R.radius0 then R.profiles.f p else Real.exp (R.logAmplitude T κ w₁ w₂ (R.logPoint p)).
Equations
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Physical U, defined pointwise by if p.1 ≤ R.radius0 then R.profiles.U p else R.axialVelocity T κ w₁ (R.logPoint p).
Equations
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Endpoint U, given by R.axialVelocity T κ w₁ (R.finalTime, η).
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Endpoint log, given by Real.log C + Real.log 220 / 2 + R.logAmplitude T κ w₁ w₂ (R.finalTime, η).
Equations
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No stock or differential equation is postulated in this constructor: the underlying profiles and all five histories are the completed REF path.
Equations
- One or more equations did not get rendered due to their size.
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The pressure and all moments are recomputed from these exact physical fields. This is the object used by the later cone and matching modules.
Equations
- One or more equations did not get rendered due to their size.
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The actual physical radial derivatives satisfy the prescribed log-clock equations. The controls use the REF stocks after REF freezes.
Quantitative conclusions for the actual integral fields. The theorem below constructs one common set of parameter thresholds for all these jets.
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The compact constants are computed from the genuine REF stocks after the reference path is fixed. Then the activation width, retained control, and both final widths can be chosen independently below positive bounds.
The same estimates stated directly for the actual physical fields.
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Direct physical error thresholds, with the reference cutoff already
fixed. Setting N = 1 supplies the value and first-parameter estimates
needed for all five histories and both lag stocks.
The bound precedes the choice of normalization C. Its only profile
input is the uniform coefficient-space ball and the proved Phi > 1/8.
Uniform higher jets before choosing the normalization #
Normalized natural log, given by Λ * realPhase h j σ η + Real.log (AxisEvaluation.profile window d.coefficients.epsilon E.coefficients.1 (Y, η)).
Equations
- One or more equations did not get rendered due to their size.
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Normalized initial, given by Real.log C + R.initialLog η.
Equations
- R.normalizedInitial C η = Real.log C + R.initialLog η
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Normalized log, given by Real.log C + R.logAmplitude T κ w₁ w₂ (y, η).
Equations
- R.normalizedLog T κ w₁ w₂ C y η = Real.log C + R.logAmplitude T κ w₁ w₂ (y, η)
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The actual held axial endpoint remains within the coefficient error and the chosen continuation error of the prescribed axial datum, in every fixed parameter derivative.
Uniform bounds for the full, actually constructed, seed. The constants
are chosen after the scale and before C; the short ramp controls are chosen
after the concrete coefficient-space solution. The bound is valid at every
nonnegative radius, so it also covers any later finite shape interval.