Actual histories of the corrected outgoing fields #
The first coordinate is the global logarithmic radius y, with normalized
X = exp y. In particular smoothness here is not smoothness at the radial
axis. Every history starts with the integral of the explicit ideal past and
then integrates the same corrected angular field and the same axial field.
The axial amplitude can be any smooth function of the parameter.
I and J omit the common physical factor sqrt 2. For arbitrary entrance
radius XR, the physical factors are XR for M,S and XR * sqrt (2*XR)
for I,J. These factors cancel from both normalized lags.
Point: an abbreviation for ℝ × ℝ.
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D Y: an abbreviation for ProfileHistories.radialPartial.
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D eta: an abbreviation for ProfileHistories.parameterPartial.
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The whole log-coordinate plane; this is not a radial domain at X=0.
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- NavierStokes.OutgoingHistories.logDomain = { carrier := Set.univ, isOpen := NavierStokes.OutgoingHistories.logDomain._proof_2, scale_mem := NavierStokes.OutgoingHistories.logDomain._proof_1 }
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A fixed incoming integral plus a finite log-coordinate integral.
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- NavierStokes.OutgoingHistories.history initial f p = initial p.2 + NavierStokes.ProfileHistories.primitive f p
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E, given by correctedAngular d w.coefficients.
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U, given by axial d.core Amp.
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H, given by Real.exp (p.1 / 2) * E w p.
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- NavierStokes.OutgoingHistories.H w p = Real.exp (p.1 / 2) * NavierStokes.OutgoingHistories.E w p
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Mass weight, given by X p * U d Amp p.
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Angular weight, given by X p * H w p.
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Transport weight, given by X p * (U d Amp p * H w p).
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Energy density, given by U d Amp p ^ 2 - E w p ^ 2 / 2.
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- NavierStokes.OutgoingHistories.energyDensity w Amp p = NavierStokes.OutgoingHistories.U d Amp p ^ 2 - NavierStokes.OutgoingHistories.E w p ^ 2 / 2
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Energy weight, given by X p * energyDensity w Amp p.
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Pressure weight, given by E w p ^ 2 / 2.
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Initial M, given by 4 * eta.
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- NavierStokes.OutgoingHistories.initialM eta = 4 * eta
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Initial I, given by (5 / 8) * d.core.P * shape eta.
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- NavierStokes.OutgoingHistories.initialI d eta = 5 / 8 * d.core.P * NavierStokes.OutgoingSchedule.shape eta
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Initial J, given by (5 / 2) * d.core.P * eta * shape eta.
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- NavierStokes.OutgoingHistories.initialJ d eta = 5 / 2 * d.core.P * eta * NavierStokes.OutgoingSchedule.shape eta
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Initial S, given by 16 * eta ^ 2 - (5 / 12) * d.core.P ^ 2 * shape eta ^ 2.
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Initial pi, given by SchedulePressure.axisPressure d eta + (5 / 2) * d.core.P ^ 2 * shape eta ^ 2.
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- NavierStokes.OutgoingHistories.initialPi d eta = NavierStokes.SchedulePressure.axisPressure d eta + 5 / 2 * d.core.P ^ 2 * NavierStokes.OutgoingSchedule.shape eta ^ 2
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I, given by history (initialI d) (angularWeight w).
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J, given by history (initialJ d) (transportWeight w Amp).
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S, given by history (initialS d) (energyWeight w Amp).
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Pi, given by history (initialPi d) (pressureWeight w).
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Transport and the two genuine lags #
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Ubar, given by M d Amp p / X p.
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Angular source as an element of ℝ.
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- One or more equations did not get rendered due to their size.
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Sq, given by angularSource w Amp p / H w p.
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Sn as an element of ℝ.
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- One or more equations did not get rendered due to their size.
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Angular stock as an element of ℝ.
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- One or more equations did not get rendered due to their size.
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Axial stock as an element of ℝ.
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- One or more equations did not get rendered due to their size.
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Qs, given by angularStock w Amp p / (X p * H w p).
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Ns, given by axialStock w Amp p / X p.
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Equation (9), with every moment and derivative constructed above.
The axial row of (9) for the same corrected fields as Qs.
The angular ODE (6), using the derivative in the true log coordinate.
The axial ODE (6); no derivative identity is an input hypothesis.
The source as printed in (6), with logarithmic derivatives written as ratios.
The incoming values and the unchanged pre-pulse region #
The incoming angular lag is fixed by the actual ideal-past integrals.
Exact endpoint cancellation for the common fields #
Identification with actual improper past integrals #
The same corrected field fixes the canonical pressure #
A left closed interval determines the derivative even at its endpoint.
Shape rate, given by 2 * eta / (1 + eta ^ 2).
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The ideal past also fixes the source primitives #
Incoming sq as an element of ℝ.
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- One or more equations did not get rendered due to their size.
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The regular source-integral definition of Q_s, including its actual past.
Incoming sn constant as an element of ℝ.
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- One or more equations did not get rendered due to their size.
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Incoming sn growing, given by d.core.P ^ 2 * shape eta ^ 2 * (5 * coordinateFactor eta * shapeRate eta + (10 * velocityExponent d.h + 1) * eta).
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- One or more equations did not get rendered due to their size.
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The regular source-integral definition of N_s, including its actual past.
Entrance-radius factors #
Physical H, given by Real.sqrt (2 * XR) * H w p.
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- NavierStokes.OutgoingHistories.physicalH XR w p = √(2 * XR) * NavierStokes.OutgoingHistories.H w p
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Physical M, given by XR * M d Amp p.
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- NavierStokes.OutgoingHistories.physicalM XR d Amp p = XR * NavierStokes.OutgoingHistories.M d Amp p
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Physical I, given by XR * Real.sqrt (2 * XR) * I w p.
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- NavierStokes.OutgoingHistories.physicalI XR w p = XR * √(2 * XR) * NavierStokes.OutgoingHistories.I w p
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Physical J, given by XR * Real.sqrt (2 * XR) * J w Amp p.
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- NavierStokes.OutgoingHistories.physicalJ XR w Amp p = XR * √(2 * XR) * NavierStokes.OutgoingHistories.J w Amp p
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Physical S, given by XR * S w Amp p.
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- NavierStokes.OutgoingHistories.physicalS XR w Amp p = XR * NavierStokes.OutgoingHistories.S w Amp p
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The common angular scaling cancels exactly from the source-integral lag.
The common axial scaling cancels exactly from the source-integral lag.
P1, given by physicalX XR p * Qs w Amp p / (1 - 2 * d.h * p.2 ^ 2).
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- NavierStokes.OutgoingHistories.p1 XR w Amp p = NavierStokes.OutgoingHistories.physicalX XR p * NavierStokes.OutgoingHistories.Qs w Amp p / (1 - 2 * d.h * p.2 ^ 2)
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P2, given by physicalX XR p * Ns w Amp p / ((1 - 2 * d.h * p.2 ^ 2) * E w p).
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- One or more equations did not get rendered due to their size.