Actual continuous cylinder L² fields for every tail grade and for the finite tail sum.
Exact residual-tail grades. Fast pressure is absent beyond degree N, and only degree N+1 retains the linear terminal corrector and slow pressure.
The existing known-jet constructor is exactly the complete finite velocity family.
Tail nonlinear field as an element of Field P T (fun z => nonlinearGrade (N+1) n (O.inverseFrame z) (O.normal z) (knownJets O (N+1) a z)).
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Tail linear field used in packet residual tail fields.
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Tail grade field as an element of Field P T (fun z => recursiveGrade O N a z n).
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- F.tailGradeField C hT Ct hCt pressure ha n hn = ((F.tailLinearField C hT Ct hCt pressure n).add (F.tailNonlinearField C n)).congr ⋯
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Tail grades, given by Ico (N+1) (2*N+3).
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- EulerPacketCylinderField.tailGrades N = Finset.Ico (N + 1) (2 * N + 3)
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Tail sum field as an element of Field P T (fun z => ∑ n ∈ tailGrades N, κ^n • recursiveGrade O N a z n).
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Prefix through, given by prefixFields (fun i hi => G i (by omega)).
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- EulerPacketCylinderField.ProfileRegularity.prefixThrough hT G = EulerPacketCylinderField.ProfileRegularity.prefixFields fun (i : ℕ) (hi : i < N + 1) => G i ⋯
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Tail grade field as an element of Field P T (fun z => recursiveGrade O N a z n).
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Tail sum field, given by (prefixThrough hT G).tailSumField C hT (G N le_rfl).correctorDerivative (G N le_rfl).corrector_time (G N le_rfl).pressure ha κ.
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