The leading stress and its genuine divergence #
The lag variables in this file are the regular primitives constructed in
ProfileHistories. Every profile and physical derivative is a Fréchet
derivative. The physical identities keep the axial-viscosity remainder.
The angular source S_q; Profiles.angularSource is H S_q.
Equations
- NavierStokes.LeadingStress.sourceTheta P h w = P.angularSource h w / P.H w
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The axial source S_n.
Equations
- NavierStokes.LeadingStress.sourceAxial P h w = P.axialSource h w
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The coefficient of the angular radial stress in Proposition 3.2.
Equations
- NavierStokes.LeadingStress.theta P h w = P.f w * w.1 * P.angularLag h w / NavierStokes.CoordinateAlgebra.L h w.2 + 2 * w.1 * NavierStokes.SimilarityProfile.partialX P.f w
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The coefficient of the axial radial stress in Proposition 3.2.
Equations
- NavierStokes.LeadingStress.axial P h w = √(2 * w.1) * (NavierStokes.SimilarityProfile.partialX P.U w + P.axialLag h w / (2 * NavierStokes.CoordinateAlgebra.L h w.2))
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Slope A, given by -2 * w.1 * partialX P.f w / P.f w.
Equations
- NavierStokes.LeadingStress.slopeA P w = -2 * w.1 * NavierStokes.SimilarityProfile.partialX P.f w / P.f w
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Slope B, given by 2 * w.1 * partialX P.U w / P.E w.
Equations
- NavierStokes.LeadingStress.slopeB P w = 2 * w.1 * NavierStokes.SimilarityProfile.partialX P.U w / P.E w
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The unweighted angular identity, using the actual regular lag equation.
The angular profile divergence in Proposition 3.2.
The axial profile divergence, obtained from the primitive-defined N_s.
The coefficient of the angular inviscid residual is the negative lag source.
The axial inviscid residual includes the actual derivative of the constructed pressure.
The exact zeroth-order transport formula. The added term is the full axial viscosity, not an estimate or a discarded remainder.
Cylindrical radial divergence (∂r + k/r)S, in the regular coordinate s=r²/2.
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The regular-coordinate radial derivative is the derivative of the actual
cylindrical slice, with the radius variable reconstructed by s=r²/2.
The physical stress scaling produces exactly the cylindrical profile divergence.
Flux profile, given by pullback h 0 (SlowDivergence.radialFlux h 0 P.U).
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Swirl profile, given by pullback h (-A h - 1 / 2) P.f.
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Axial profile, given by pullback h (-A h) P.U.
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Pressure profile, given by pullback h (-2 * A h) P.pressure.
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Physical stress theta, given by pullback h (-A h - 1 / 2) (theta P h).
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Physical stress axial, given by pullback h (-A h - 1 / 2) (axial P h).
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Physical velocity, given by AxisymmetricResidual.velocity (RadialFluxResidual.radialB (fluxProfile P h)) (swirlProfile P h) (axialProfile P h).
Equations
- One or more equations did not get rendered due to their size.
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Physical pressure, given by AxisymmetricResidual.pressure (pressureProfile P h).
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The angular axial-viscosity term omitted from the leading radial balance.
Equations
- One or more equations did not get rendered due to their size.
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The axial axial-viscosity term omitted from the leading radial balance.
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The regular swirl coefficient reconstructs precisely u_theta=q^(-A) E.
Cylindrical angular component of a genuine Cartesian vector.
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Proposition 3.2 for the actual Cartesian Navier--Stokes residual.
The local hypotheses avoid extending the quotient defining radial velocity
across the axis. The two added terms are the exact axial-viscosity terms;
their explicit similarity formulas are thetaAxialViscosity_eq and
axialAxialViscosity_eq.