The actual outgoing tail and its cone estimates #
The controller below is identified with an actual corrected angular history
by ReleaseMoments. Bounds never assume an amplitude small relative to h:
the prescribed long release plateau supplies that suppression.
Pressure through the actual angular reset #
The corrected pressure is the improper integral of the actual corrected field. The difference from the clean pressure is an explicit finite partial-reset integral. Bounds use the first angular coefficient jet supplied by the proved reset witness; no parity or second-jet estimate is assumed.
Corrected pi, given by -(1 / 2 : ℝ) * ∫ t in Ioi y, correctedAngular d w.coefficients (t, eta) ^ 2.
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- NavierStokes.CorrectedPressureBounds.correctedPi w y eta = -(1 / 2) * ∫ (t : ℝ) in Set.Ioi y, NavierStokes.UniformAngularReset.correctedAngular d w.coefficients (t, eta) ^ 2
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Edit density, given by correctedAngular d w.coefficients p ^ 2 - finalAngular d p ^ 2.
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Edit size, given by K * d.core.lam ^ (28 : ℕ).
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Edit density eta, constructed using 2.
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- One or more equations did not get rendered due to their size.
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Pressure change, given by correctedPi w y eta - Pi d y eta.
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The edit derivative is controlled by the actual local corrected field.
Canonical forward pressure with the unchanged whole-axis pressure datum.
Release lower constant, given by min (Real.exp (-2)) (Real.exp (-1) * tailCoefficient).
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Positivity of the actual angular-history lag through the first half tail unit.
The designed suppression of the actual field #
Future integrals on the uniform release #
The backward-energy numerator in the uniform region. Its identification with the source primitive uses the actual zero total energy.
Equations
- NavierStokes.TailCone.releaseNumerator d eta y = 2 * eta * (d.h * NavierStokes.TailCone.releaseFutureEnergy d y - (1 / 2 + d.h) * NavierStokes.TailCone.releaseFutureMass d y)
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Numerator constant, given by 2 * (1 + FuturePressureBounds.envelopeConstant).
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Uniform smallness after dividing by the actual controller #
Release velocity ratio, given by releaseNumerator d eta y / (finalAngular d (y, 0) * ReleaseMoments.normalizedLag d c eta y).
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- One or more equations did not get rendered due to their size.
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Release cone constant, given by (earlyRatioConstant + lateRatioConstant) * (P * Real.exp (Real.exp m + 12)).
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Actual slopes and the finite stress cone #
Release P1, given by XR * Real.exp y * ReleaseMoments.normalizedLag d c eta y / CoordinateAlgebra.L d.h eta.
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- NavierStokes.TailCone.releaseP1 d c XR eta y = XR * Real.exp y * NavierStokes.ReleaseMoments.normalizedLag d c eta y / NavierStokes.CoordinateAlgebra.L d.h eta
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Release radius threshold, given by 16 / (Real.exp d.releaseStart * (releaseLowerConstant * d.h)).
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Identification with the actual global histories #
Zero actual total energy fixes the future energy term, including the reset.
Actual logarithmic derivatives through flattening and reset #
Reset relative, given by relative (w.coefficients eta) (y - correctionCenter d).
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Reset radial derivative, given by deriv (relative (w.coefficients eta)) (y - correctionCenter d).
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Reset eta derivative, given by relative (deriv w.coefficients eta) (y - correctionCenter d).
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Corrected flat slope, given by `flatteningSlope d y eta + resetRadialDerivative w eta y / (1
- resetRelative w eta y)`.
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- One or more equations did not get rendered due to their size.
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Corrected eta slope, given by etaRate d eta y + resetEtaDerivative w eta y / (1 + resetRelative w eta y).
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- One or more equations did not get rendered due to their size.
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Reset source error, given by (2 * resetJetConstant + 2) * (K * d.core.lam ^ (28 : ℕ)).
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- NavierStokes.TailCone.resetSourceError d K = (2 * NavierStokes.TailCone.resetJetConstant + 2) * (K * d.core.lam ^ 28)
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Energy and its parameter derivative on the finite post-pulse interval #
Finite energy budget, given by `flattenLength + releaseConstant + 40 + 20 * (d.releaseStart
- d.core.endpoint)`.
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Finite numerator budget, given by 5 * finiteEnergyBudget d + 12 * CorrectedPressureBounds.correctedConstant.
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Finite numerator constant, given by 5 * (flattenLength + releaseConstant + 40 + 20 * (flattenLength + 30)) + 12 * CorrectedPressureBounds.correctedConstant.
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- One or more equations did not get rendered due to their size.
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A lower amplitude bound up to release #
The finite waiting interval loses only eighteen powers of lam, whereas the
earlier scheduled wait has already supplied thirty powers.
Finite amplitude constant, given by Real.exp (-(3 / 5 : ℝ) * flattenLength) / 4.
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Finite cone constant, given by `(4 * finiteNumeratorConstant / finiteAmplitudeConstant) * (P
- Real.exp (Real.exp m + 12))`.
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Cone quantities of the actual corrected profile #
Actual A, given by 1 - 2 * deriv (fun t => Real.log (OutgoingHistories.E w (t, eta))) y.
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Actual bs, given by 2 * deriv (fun t => OutgoingHistories.U d Amp (t, eta)) y / OutgoingHistories.E w (y, eta).
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- NavierStokes.TailCone.actualBs w Amp y eta = 2 * deriv (fun (t : ℝ) => NavierStokes.OutgoingHistories.U d Amp (t, eta)) y / NavierStokes.OutgoingHistories.E w (y, eta)
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Finite radius threshold, given by 16 / (Real.exp d.core.endpoint * (d.core.lam / 4)).
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Tail radius threshold, given by max (finiteRadiusThreshold d) (releaseRadiusThreshold d).
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All quantities are those of the corrected profile and its actual integral histories. The scalar smallness conditions are arranged by the thresholds below.
Simultaneous parameter choice, uniform in the terminal parameter #
The post-pulse pointwise cone for the exact corrected schedule.
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- One or more equations did not get rendered due to their size.
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A common positive lam threshold works for every 0 < 2*h < lam.
The entrance radius is chosen only after the full schedule, including h.
No energy, pressure, angular-lag, or cone inequality is assumed as input.