Actual terminal stress factors at the outer edge #
The logarithmic edge coordinate is applied to the actual physical heat carrier
and to OutgoingTail.tailShape. A positive global physical chart keeps the
parameter coefficients smooth without assuming a normalized stress factor.
Edge param: an abbreviation for ℝ × ℝ.
Equations
Instances For
Axis point, given by (timeOf p, (0, p.2)).
Equations
Instances For
Chart Q, given by SimilarityProfile.q d.h (axisPoint p).
Equations
Instances For
Chart eta, given by SimilarityProfile.eta d.h (axisPoint p).
Equations
Instances For
Outer radius, given by Real.sqrt (2 * chartQ d p * Real.exp (y0 + 3)).
Equations
- NavierStokes.TerminalEdgeFactor.outerRadius d y0 p = √(2 * NavierStokes.TerminalEdgeFactor.chartQ d p * Real.exp (y0 + 3))
Instances For
Radius, given by outerRadius d y0 y.1 * Real.exp (-y.2 / 2).
Equations
- NavierStokes.TerminalEdgeFactor.radius d y0 y = NavierStokes.TerminalEdgeFactor.outerRadius d y0 y.1 * Real.exp (-y.2 / 2)
Instances For
Chart point, given by radiusPoint (timeOf y.1) (radius d y0 y) y.1.2.
Equations
Instances For
Carrier, given by physicalHeat C (1 + d.h) (chartPoint d y0 y).
Equations
- NavierStokes.TerminalEdgeFactor.carrier C d y0 y = NavierStokes.TerminalStress.physicalHeat C (1 + d.h) (NavierStokes.TerminalEdgeFactor.chartPoint d y0 y)
Instances For
Carrier radial, given by radius d y0 y * SimilarityProfile.partialS (physicalHeat C (1 + d.h)) (chartPoint d y0 y).
Equations
- One or more equations did not get rendered due to their size.
Instances For
Denominator, given by timeDenominator d.h (timeOf p) p.2.
Equations
Instances For
A radial logarithmic distance, with its outer radius kept explicit.
Equations
- NavierStokes.TerminalEdgeFactor.edgeCoordinate R r = -2 * Real.log (r / R)
Instances For
Continuous positive-radius functions with a zero tail are genuinely integrable.
An actual radial-to-edge change of variables, proved by the improper FTC.
Log taper, given by tailShape d (y - y0).
Equations
Instances For
Radial taper, given by radialSlice (flattening d.h (logTaper d y0)) (timeOf p) p.2.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Boundary coefficient, given by (2 * carrier C d y0 y / radius d y0 y) * taperSlopeFactor d y.2.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Time coefficient, given by `(radius d y0 y ^ 3 * carrier C d y0 y / (2 * denominator d y.1))
- taperSlopeFactor d y.2`.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Correction coefficient, given by (radius d y0 y * carrier C d y0 y - radius d y0 y ^ 2 * carrierRadial C d y0 y) * taperSlopeFactor d y.2.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Angular stress, given by terminalStress C d.h (logTaper d y0) (timeOf y.1) y.1.2 (radius d y0 y).
Equations
- One or more equations did not get rendered due to their size.
Instances For
Angular factor, constructed using boundaryCoefficient.
Equations
- One or more equations did not get rendered due to their size.
Instances For
The leading angular stress itself, with all backward-integral hypotheses proved for the actual heat carrier and actual outgoing taper.
The same edge coordinate in the regular radial variable s=r²/2.
Equations
Instances For
Outer S, given by chartQ d p * Real.exp (y0 + 3).
Equations
- NavierStokes.TerminalEdgeFactor.outerS d y0 p = NavierStokes.TerminalEdgeFactor.chartQ d p * Real.exp (y0 + 3)
Instances For
Chi, given by 2 * chartEta d p / (chartQ d p ^ CoordinateAlgebra.D d.h * CoordinateAlgebra.L d.h (chartEta d p)).
Equations
- One or more equations did not get rendered due to their size.
Instances For
Pressure coefficient, given by carrier C d y0 y ^ 2 * tailShape d (3 - y.2) * taperSlopeFactor d y.2.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Pressure factor, given by chi d y.1 * ParametricFlatFactor.factor 4 3 (pressureCoefficient C d y0) y.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Axial coefficient, given by (radius d y0 y ^ 2 / 2) * pressureFactor C d y0 y.
Equations
- NavierStokes.TerminalEdgeFactor.axialCoefficient C d y0 y = NavierStokes.TerminalEdgeFactor.radius d y0 y ^ 2 / 2 * NavierStokes.TerminalEdgeFactor.pressureFactor C d y0 y
Instances For
Axial factor, given by ParametricFlatFactor.factor 4 0 (axialCoefficient C d y0) y / radius d y0 y.
Equations
- One or more equations did not get rendered due to their size.
Instances For
The actual canonical pressure gradient on the physical chart.
Equations
- One or more equations did not get rendered due to their size.
Instances For
The actual axial backward stress, written in the regular radius s=r²/2.
Equations
- One or more equations did not get rendered due to their size.
Instances For
A profile chart including both endpoints η = ±1 #
These expressions use the actual heat profile on |η| ≤ 1. Its proven
smooth extension and a positive extension of L supply coefficients on a
neighborhood of that closed interval. No value of the implicit coordinates
at zero backward time is used.
Positive extension, given by m / 2 + (x - m / 2) * OutgoingSchedule.sigma ((x - m / 2) / (m / 2)).
Equations
Instances For
Profile L, given by positiveExtension (1 - 2 * d.h) (CoordinateAlgebra.L d.h η).
Equations
Instances For
Profile Z, given by 2 * (1 - y.1 ^ 2) / profileS y0 y.2.
Equations
- NavierStokes.TerminalEdgeFactor.profileZ y0 y = 2 * (1 - y.1 ^ 2) / NavierStokes.TerminalEdgeFactor.profileS y0 y.2
Instances For
Profile carrier, given by C * (profileS y0 y.2) ^ RadialHeatProfile.spatialExponent (1 + d.h) * HeatProfileExtension.extension (1 + d.h) (profileZ y0 y).
Equations
- One or more equations did not get rendered due to their size.
Instances For
Profile carrier radial, constructed using C.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Profile boundary coefficient, given by `(2 * profileCarrier C d y0 y / profileRadius y0 y.2)
- taperSlopeFactor d y.2`.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Profile time coefficient, given by `(profileRadius y0 y.2 ^ 3 * profileCarrier C d y0 y / (2
- profileL d y.1)) * taperSlopeFactor d y.2`.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Profile correction coefficient as an element of ℝ.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Profile angular factor, constructed using profileBoundaryCoefficient.
Equations
- One or more equations did not get rendered due to their size.
Instances For
The boundary term and the two actual terminal primitives in profile coordinates.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Profile pressure coefficient, given by `profileCarrier C d y0 y ^ 2 * tailShape d (3 - y.2)
- taperSlopeFactor d y.2`.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Profile pressure factor, given by profileChi d y.1 * ParametricFlatFactor.factor 4 3 (profilePressureCoefficient C d y0) y.
Equations
- One or more equations did not get rendered due to their size.
Instances For
The first genuine terminal primitive, before any factorization.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Profile axial coefficient, given by profileS y0 y.2 * profilePressureFactor C d y0 y.
Equations
Instances For
Profile axial factor, given by ParametricFlatFactor.factor 4 0 (profileAxialCoefficient C d y0) y / profileRadius y0 y.2.
Equations
- One or more equations did not get rendered due to their size.
Instances For
The second terminal primitive is the integral of the first one, with
the exact Jacobian s = exp(Y-δ) of the regular radial coordinate.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Identification of both physical pressure primitives #
Agreement with the physical section away from the endpoints #
Full profile stress, all jets, and the edge direction #
Profile stress, given by (profileAngularStress C d y0 y, profileAxialStress C d y0 y).
Equations
Instances For
Profile stress factor, given by (profileAngularFactor C d y0 y, y.2 ^ 6 * profileAxialFactor C d y0 y).
Equations
- One or more equations did not get rendered due to their size.
Instances For
Actual full tensors, uniformly through both endpoints of the profile interval.
Profile tilt, given by y.2 ^ 6 * profileAxialFactor C d y0 y / profileAngularFactor C d y0 y.
Equations
- NavierStokes.TerminalEdgeFactor.profileTilt C d y0 y = y.2 ^ 6 * NavierStokes.TerminalEdgeFactor.profileAxialFactor C d y0 y / NavierStokes.TerminalEdgeFactor.profileAngularFactor C d y0 y
Instances For
The actual velocity shear ratio for the terminal product K f_o.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Profile domain, given by {y | profileCarrier C d y0 y ≠ 0}.
Equations
Instances For
Profile cone gap, given by 2 - (profileSpeed C d y0 y - 2) * profileTilt C d y0 y ^ 2.
Equations
- NavierStokes.TerminalEdgeFactor.profileConeGap C d y0 y = 2 - (NavierStokes.TerminalEdgeFactor.profileSpeed C d y0 y - 2) * NavierStokes.TerminalEdgeFactor.profileTilt C d y0 y ^ 2
Instances For
One strict relative cone margin on a collar, uniformly for -1 ≤ η ≤ 1.
The shear is the finite, actual terminal velocity shear; its value is proved
strictly larger than two on the boundary.
The shear formula is the derivative of the actual profile velocity #
Profile angular velocity, given by profileCarrier C d y0 y * tailShape d (3 - y.2).
Equations
Instances For
Since δ=Y-2 log r, 1+2 ∂δ log(K f_o) is exactly the radial shear
1-r ∂r(K f_o)/(K f_o). Here its logarithmic derivative is proved directly.
The strict cone inequalities for the actual stress hold throughout one positive-width terminal collar, uniformly through the closed profile interval.
The same weighted estimates on compact physical parameter sets #
Physical stress, given by (angularStress C d y0 y, axialStress C d y0 y).
Equations
Instances For
Physical stress factor, given by (angularFactor C d y0 y, y.2 ^ 6 * axialFactor C d y0 y).
Equations
- NavierStokes.TerminalEdgeFactor.physicalStressFactor C d y0 y = (NavierStokes.TerminalEdgeFactor.angularFactor C d y0 y, y.2 ^ 6 * NavierStokes.TerminalEdgeFactor.axialFactor C d y0 y)
Instances For
The genuine root-form cone on the terminal collar #
Profile swirl coefficient, given by profileAngularVelocity C d y0 y / profileRadius y0 y.2.
Equations
Instances For
Profile P, given by profileSpeed C d y0 y + profileAngularStress C d y0 y / profileSwirlCoefficient C d y0 y.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Profile J, given by profileAxialStress C d y0 y / profileSwirlCoefficient C d y0 y.
Equations
Instances For
Applying the exact true-cone equivalence to the actual terminal stress,
with P-v=Tθ/F and J=Tz/F, rather than taking a large-amplitude limit.