The actual pulse contribution to the outgoing stress cone #
The endpoint lower bound, pulse stress expansions, and numerical cone margins are derived from the actual corrected fields and their histories. One small-parameter threshold preserves every prechosen reset witness.
The actual outgoing pulse lag #
The exponential convolution is expanded by two integrations by parts. The resulting remainder is controlled by the actual second derivative of the forcing, with constants uniform in the pulse duration.
Lag, given by m₀ * Real.exp (-β * y) + convolution β f y.
Equations
- NavierStokes.PulseLag.lag β m₀ f y = m₀ * Real.exp (-β * y) + NavierStokes.PulseLag.convolution β f y
Instances For
Exact second-order integration-by-parts identity, including the initial boundary terms.
Main second bound, choosing the witness provided by
LocalizedMomentRepair.smooth_compact_derivative_bound.
Equations
Instances For
Forcing, given by A * mainPulse (c.lam * y) + affineProfile c q A y.
Equations
- NavierStokes.PulseLag.forcing c q A y = A * NavierStokes.OutgoingSchedule.mainPulse (c.lam * y) + NavierStokes.OutgoingPulseBounds.affineProfile c q A y
Instances For
The actual radial mass average divided by the actual angular profile,
at pulse-relative log time y.
Equations
- One or more equations did not get rendered due to their size.
Instances For
The exact exponential-convolution representation of the actual lag; it is derived from the radial mass integral.
The actual mass lag satisfies the pulse ODE, including its right derivative at pulse time zero.
Affine error, constructed using affineLag.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Error in the two-term expansion of the actual normalized mass lag, with its exact exponentially decaying initial value retained.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Scaled pulse, given by pulseRatio c amp (z / c.lam, eta).
Equations
- NavierStokes.PulseLag.scaledPulse c amp eta z = NavierStokes.OutgoingSchedule.pulseRatio c amp (z / c.lam, eta)
Instances For
Full error, constructed using normalizedLag.
Equations
- One or more equations did not get rendered due to their size.
Instances For
A common explicit constant bounds the actual lag error and its first parameter derivative on the full nonnegative pulse-time half-line.
The concrete energy-closing amplitude satisfies the lag estimate.
One positive threshold and one constant, selected before lambda, control the lag and its first parameter derivative throughout the pulse.
The same lag estimate for the amplitude which closes the energy after the actual angular-moment reset.
The corrected amplitude and reset witness are actually constructed by
exists_corrected_amplitude; an additional fixed threshold makes their
first derivative at most one. The common lag constant is independent of
lambda, the terminal parameter, eta, and pulse time.
Actual outgoing energy histories during the pulse #
The history and its parameter derivative retain the actual incoming prefix. Bounds come from their source integrals and the explicit pulse energy weight.
Pulse normalization, given by PulseAmplitude.normalization c * shape eta ^ 2.
Equations
Instances For
The actual reset leaves the pulse angular field unchanged.
Exact source of the actual energy history throughout the pulse.
Exact parameter derivative of the pulse energy source.
The pulse starts with the actual incoming energy, including the ideal past.
The actual energy source and its actual parameter derivative have a common bound.
Prefix bounds include the incoming ideal history and its parameter derivative.
Integrating an actual history source over a pulse of length 13 / lam.
The final denominator is its exponentially decaying pulse energy weight.
Genuine normalized energy-history bounds from explicit pulse-ratio data. No energy-history estimate appears among the hypotheses.
A common bound for the main pulse and its actual affine moment repair.
Equations
Instances For
The parameter derivative includes the derivative of the actual moment repair.
This constant depends only on the fixed parameters P,m.
Equations
- NavierStokes.PulseEnergyHistory.historyConstant P m = 16 * NavierStokes.PulseAmplitude.prefixBoundConstant P m + 13 * (6 * (6 * NavierStokes.PulseEnergyHistory.forceConstant P m) ^ 2 + 2)
Instances For
Both requested actual history bounds, with the actual repaired pulse source.
Specialization to the corrected amplitude supplied by the proved energy solve.
Force constant, given by mainBound + correctionJetBound P m 0.
Equations
Instances For
Uniform bounds for the actual pulse ratio, normalized mass history, and its first parameter derivative.
Shape gradient, given by 2 * eta / (1 + eta ^ 2).
Instances For
Pulse angular source as an element of ℝ.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Source constant, given by energyConstant P m * (4 * averageConstant P m + 18 * forceConstant P m).
Equations
Instances For
A lower barrier for the exact scalar lag equation on a finite interval. Only the differential equation and a lower source bound are used.
The long actual pulse turns a nonnegative incoming angular lag and
the lower source 3*lambda/8 into the endpoint bound needed by the tail.
Binding the pulse formulas to the actual corrected histories #
One-sided equality before the endpoint determines the true radial derivative there as well, since both profiles are smooth.
The source estimate is for the actual stress history: no source formula or lag approximation is an input.
The actual angular lag at the endpoint, initially conditional only on its incoming sign and explicit schedule/amplitude bounds.
A positive threshold selected from the two fixed prefix parameters.
Equations
- NavierStokes.PulseCone.sourceThreshold P m = min (1 / 120) (1 / (8 * NavierStokes.PulseCone.sourceConstant P m))
Instances For
Exact stability estimate for a scalar lag around a constant source. The source error is allowed to have either sign.
Uniform angular-lag error throughout the actual pulse; the incoming error is retained explicitly for the shaped-wait theorem to supply.
The actual endpoint lower bound follows from the constructed incoming history and numerical parameter restrictions, with no incoming-lag or source estimate assumed.
The final energy-closing amplitude, including the angular reset, is the amplitude used in this endpoint theorem.
The axial identity and the genuine pressure remainder #
Axial history error as an element of ℝ.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Exact substitution in the integrated axial stress. The error is an explicit expression in the same constructed energy and pressure histories.
Uniform value and first parameter derivative bounds for the actual canonical pressure throughout the pulse.
Actual viscous coefficients on the pulse #
Radial A, given by 2 - 2 * (dY (H w) p / H w p).
Equations
Instances For
Shear B, given by 2 * dY (U d amp) p / E w p.
Equations
Instances For
Direction ratio, given by Ns w amp p / (E w p * Qs w amp p).
Equations
- NavierStokes.PulseCone.directionRatio w amp p = NavierStokes.OutgoingHistories.Ns w amp p / (NavierStokes.OutgoingHistories.E w p * NavierStokes.OutgoingHistories.Qs w amp p)
Instances For
Quantitative pulse jets and parameter sensitivity #
Only this upper derivative bound is used for the favorable cutoff sign.
Main first bound, choosing the witness provided by
LocalizedMomentRepair.smooth_compact_derivative_bound.
Equations
Instances For
Value repair constant, given by 384 * correctionJetBound P m 0.
Equations
Instances For
Derivative repair constant, given by 384 * correctionJetBound P m 1.
Equations
Instances For
Derivative constant, given by 2 * mainFirstBound + derivativeRepairConstant P m.
Equations
Instances For
Parameter lag constant, given by 4 * prefixBound P m 0 + 960 * correctionJetBound P m 0.
Equations
Instances For
The parameter derivative has the small amplitude-derivative factor; the remaining dependence is quadratically small in lambda.
The coefficient in the pulse-direction expansion #
Geometric source, given by (1 / 2 - d.h) * eta * shapeGradient eta.
Equations
- NavierStokes.PulseCone.geometricSource d eta = (1 / 2 - d.h) * eta * NavierStokes.PulseCone.shapeGradient eta
Instances For
Equilibrium numerator, given by d.core.lam - d.h + geometricSource d eta.
Equations
- NavierStokes.PulseCone.equilibriumNumerator d eta = d.core.lam - d.h + NavierStokes.PulseCone.geometricSource d eta
Instances For
Angular equilibrium, given by equilibriumNumerator d eta / (1 - d.core.lam).
Equations
- NavierStokes.PulseCone.angularEquilibrium d eta = NavierStokes.PulseCone.equilibriumNumerator d eta / (1 - d.core.lam)
Instances For
Derivative coefficient, given by `d.core.lam * ((1 / 2 - d.h) + geometricSource d eta) * (1
- d.core.lam) / (decay d.core ^ 2 * equilibriumNumerator d eta)`.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Main direction as an element of ℝ.
Equations
- One or more equations did not get rendered due to their size.
Instances For
The actual mass expansion is inserted into the actual axial history.
Strict numerical margins, stable under quantified errors #
Cone error budget, given by `2 * eps * (M + F + 1) + eps * (2 * F + 1) / 2 + 2 * lam * (M +
- ^ 2`.
Equations
Instances For
A completely numerical perturbation lemma. The actual profile estimates below supply both errors and the small budget.
The axial history error is derived from actual moments #
Axial error constant, constructed using energyConstant.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Division by the angular lag near the equator #
Main direction bound, given by 18 * forceConstant P m + 3 * derivativeConstant P m.
Equations
Instances For
A quantified division step retaining every error term. Its two angular-lag hypotheses are supplied by the shaped-wait estimate.
Main ratio, given by amp eta * mainPulse (c.lam * y).
Equations
- NavierStokes.PulseCone.mainRatio c amp eta y = amp eta * NavierStokes.OutgoingSchedule.mainPulse (c.lam * y)
Instances For
Main slope, given by amp eta * deriv mainPulse (c.lam * y).
Equations
- NavierStokes.PulseCone.mainSlope c amp eta y = amp eta * deriv NavierStokes.OutgoingSchedule.mainPulse (c.lam * y)
Instances For
Ideal direction, given by 2 * mainRatio d.core amp eta y - derivativeCoefficient d eta * mainSlope d.core amp eta y.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Main ratio bound, given by 2 * mainBound.
Instances For
Shear error constant, given by valueRepairConstant P m + 2 * derivativeConstant P m + 12 * forceConstant P m.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Direction main error constant, given by 18 * forceConstant P m + 2 * valueRepairConstant P m + 3 * derivativeRepairConstant P m.
Equations
- One or more equations did not get rendered due to their size.
Instances For
The shaped wait supplies the actual angular equilibrium error #
The equilibrium approximation now has no initial-error hypothesis.
A single explicit vanishing rate for the cone errors #
Direction error constant, constructed using 4.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Component constant, given by `directionErrorConstant P m A + directionMainErrorConstant P m
- shearErrorConstant P m + 1`.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Pulse budget, given by coneErrorBudget mainRatioBound idealDirectionBound (componentConstant P m A * coneRate lam) lam.
Equations
- One or more equations did not get rendered due to their size.
Instances For
The numerical margins refer only to the actual global stress histories and the actual first radial derivatives of the corrected fields.
Instances For
The full pulse cone for any smooth amplitude with the proved size and first-derivative rate. Every further hypothesis is a scalar parameter bound.
Amplitude derivative constant, given by 128 * CorrectedPulseAmplitude.combinedConstant P m K.
Equations
Instances For
Corrected pulse budget, given by pulseBudget P m (amplitudeDerivativeConstant P m K) lam.
Equations
Instances For
The full actual pulse cone for the same corrected amplitude and reset witness as the global schedule. No stress or cone estimate is assumed.
One threshold is chosen after the fixed prefix and reset constant. It works for every supplied reset witness, keeps its actual energy-closing amplitude, and is uniform over the full pulse and the physical parameter band.