The first slow-order stress at the terminal edge #
The source is the angular axial-viscosity term. Its primitive is the actual
backward integral with weight R². The coefficient chart is (η,δ), including
both endpoints η=±1; its heat carrier uses the genuine smooth heat extension.
Taper second factor, given by `-8 * taperSlopeFactor d x + 3 * x ^ 2 * taperSlopeFactor d x
- x ^ 3 * deriv (taperSlopeFactor d) x`.
Equations
- One or more equations did not get rendered due to their size.
Instances For
The normalized negative axial-viscosity source, before radial integration.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Source factor, given by -profileCarrier C d y0 y * (profileChi d y.1 ^ 2 * taperSecondFactor d y.2 + beta d y.1 * y.2 ^ 3 * taperSlopeFactor d y.2).
Equations
- One or more equations did not get rendered due to their size.
Instances For
Primitive coefficient, given by (profileRadius y0 y.2 ^ 3 / 2) * sourceFactor C d y0 y.
Equations
Instances For
The source in the positive normalized radial variable R=√(2X).
Equations
- One or more equations did not get rendered due to their size.
Instances For
The genuine backward weighted radial primitive, with the stress sign convention.
Equations
Instances For
Profile stress, given by radialStress C d y0 y.1 (profileRadius y0 y.2).
Equations
Instances For
Stress factor, given by ParametricFlatFactor.factor 4 6 (primitiveCoefficient C d y0) y / profileRadius y0 y.2 ^ 2.
Equations
- One or more equations did not get rendered due to their size.
Instances For
All full joint derivative tensors, uniformly including both parameter endpoints.
The actual (X,η) profile coordinates #
Stress X, given by profileStress C d y0 (xChart y0 w).
Equations
Instances For
The two logarithmic Gaussian factors specified in (20).
Equations
- NavierStokes.SlowFirstOrderEdge.zeta cL a y0 X = NavierStokes.FlatCutoff.edge cL (Real.log (X / a)) * NavierStokes.FlatCutoff.edge 4 (y0 + 3 - Real.log X)
Instances For
The full weight from (20), with the lesser of the two log distances and one. The only geometric condition is that the closed outer collar avoids the inner edge.
Literal axial derivatives in physical coordinates #
Physical point: an abbreviation for SimilarityProfile.PhysicalPoint.
Equations
Instances For
Physical chi, given by q d.h p ^ (-CoordinateAlgebra.D d.h) * profileChi d (eta d.h p).
Equations
- One or more equations did not get rendered due to their size.
Instances For
Physical taper, given by tailShape d (Real.log (X d.h p) - y0).
Equations
Instances For
Literal physical angular velocity on the switched terminal collar.
Equations
Instances For
Literal negative second axial derivative; no independent jet is supplied.
Equations
Instances For
The residual order is q^(-A-1+2h), before one radial integration.
Physical scale, given by q d.h (t, (0, z)).
Equations
Instances For
Physical eta, given by eta d.h (t, (0, z)).
Equations
Instances For
Physical stress, given by backwardStress (fun u => physicalSource C d y0 (radiusPoint t u z)) r.
Equations
- One or more equations did not get rendered due to their size.
Instances For
Identification of the actual physical backward primitive with the first-order profile coefficient, using the manuscript's exact tensor power.
Global moment closure is supplied by the separate renormalized-moment and slow-order moment theorems. Only agreement on the exterior ray is needed here.
The literal terminal velocity is the actual fully switched heat edit from the outgoing schedule, with its original amplitude and log origin.