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Add C¹-continuous Hermite spline bridge for 16D Reynolds regime transition
Implements the UniversalBridge module in Lean with Q16.16 fixed-point arithmetic, connecting the laminar exit (Re=2300, f=0.0278) and turbulent entry (Re=4000, f=0.0398) with provable C¹ continuity. Includes 24 verification theorems (boundary conditions, basis function values, regime classification, controller gate semantics) and 10 executable #eval! witnesses as computational receipts.
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@ -4,5 +4,6 @@ import Semantics.Physics.Conservation
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import Semantics.Physics.Interaction
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import Semantics.Physics.Projection
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import Semantics.Physics.Examples
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import Semantics.Physics.UniversalBridge
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import Semantics.Physics.BindPhysics
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import Semantics.Physics.Tests
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@ -0,0 +1,321 @@
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/-
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UniversalBridge.lean - Hermite Spline Transition for the 16D Reynolds Regime Bridge
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Implements the C¹-continuous Cubic Hermite Spline connecting the laminar and
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turbulent friction-factor regimes across the transitional zone (2300 ≤ Re ≤ 4000).
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Boundary conditions (Moody chart / Darcy friction factor):
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Point A (Laminar exit): Re=2300, f=0.0278, slope m₀ = −1.21×10⁻⁵
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Point B (Turbulent entry): Re=4000, f=0.0398, slope m₁ = −2.49×10⁻⁶
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The bridge function H(t) uses the normalized variable t = (Re − 2300) / 1700
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and satisfies:
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H(0) = y₀, H'(0) = h·m₀
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H(1) = y₁, H'(1) = h·m₁
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Intermittency γ = (H(t) − y₀) / (y₁ − y₀) gives the turbulent fraction in
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the 16D controller's superpositional collapse model.
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Note on Q16.16 arithmetic:
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Lean 4.30 uses Euclidean (floor) division for `Int./`. Standard Q16.16
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multiplication truncates toward zero. We correct this via an explicit
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sign check in `q16_mul`. The difference is at most 1 ULP (1/65536)
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and is negligible for engineering purposes, but formal correctness
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requires the fix.
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-/
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namespace Semantics.Physics.UniversalBridge
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-- ============================================================================
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-- Q16.16 fixed-point scale (2¹⁶ = 65536)
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-- ============================================================================
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def SCALE : Int := 65536
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-- ============================================================================
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-- Boundary condition constants (all pre-computed as Q16.16 integers)
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-- ============================================================================
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/-- Reynolds number at laminar exit -/
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def RE_LAMINAR : Int := 2300
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/-- Reynolds number at turbulent entry -/
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def RE_TURBULENT : Int := 4000
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/-- Interval width h = RE_TURBULENT − RE_LAMINAR = 1700 -/
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def H_INTERVAL : Int := 1700
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/-- f at laminar exit: round(0.0278 × 65536) = 1822 -/
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def Y0 : Int := 1822
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/-- f at turbulent entry: round(0.0398 × 65536) = 2608 -/
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def Y1 : Int := 2608
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/-- h·m₀ where m₀ = −1.21e−5: round(1700 × −1.21e−5 × 65536) = −1348 -/
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def H_M0 : Int := -1348
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/-- h·m₁ where m₁ = −2.49e−6: round(1700 × −2.49e−6 × 65536) = −277 -/
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def H_M1 : Int := -277
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-- ============================================================================
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-- Q16.16 arithmetic helpers
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-- ============================================================================
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/-- Q16.16 multiplication with truncation toward zero.
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Lean's `Int./` is Euclidean division (floor), which rounds negative
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results one further away from zero. We correct by negating the
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truncation of the absolute product. -/
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def q16_mul (a b : Int) : Int :=
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let prod := a * b
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if prod ≥ 0 then prod / SCALE else -((-prod) / SCALE)
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def q16_add (a b : Int) : Int := a + b
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def q16_sub (a b : Int) : Int := a - b
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/-- Q16.16 division guarded against division by zero. Returns `none` when
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divisor is zero. Euclidean division is acceptable here because the
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result is always non-negative for valid Reynolds inputs. -/
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def q16_div (a b : Int) : Option Int :=
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if b = 0 then none else some ((a * SCALE) / b)
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-- ============================================================================
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-- Normalized variable t = (Re − 2300) / 1700, as Q16.16
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-- ============================================================================
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def normalizedT (re : Int) : Option Int :=
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if re < RE_LAMINAR then some 0
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else if re > RE_TURBULENT then some SCALE
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else q16_div (re - RE_LAMINAR) H_INTERVAL
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-- ============================================================================
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-- Hermite basis functions (all operate on Q16.16 t ∈ [0, SCALE])
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-- ============================================================================
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/-- Basis function h00(t) = (1 − t)²(1 + 2t) = 1 − 3t² + 2t³ -/
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def h00 (t : Int) : Int :=
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let t2 := q16_mul t t
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let t3 := q16_mul t2 t
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let term3 := q16_mul (3 * SCALE) t2
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let term2 := q16_mul (2 * SCALE) t3
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q16_sub (q16_add SCALE term2) term3
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/-- Basis function h01(t) = t²(3 − 2t) = 3t² − 2t³ -/
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def h01 (t : Int) : Int :=
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let t2 := q16_mul t t
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let t3 := q16_mul t2 t
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let term3 := q16_mul (3 * SCALE) t2
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let term2 := q16_mul (2 * SCALE) t3
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q16_sub term3 term2
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/-- Basis function h10(t) = (1 − t)²·t -/
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def h10 (t : Int) : Int :=
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let t1m := q16_sub SCALE t
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let t1m2 := q16_mul t1m t1m
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q16_mul t1m2 t
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/-- Basis function h11(t) = t²·(1 − t) -/
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def h11 (t : Int) : Int :=
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let t2 := q16_mul t t
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let t1m := q16_sub SCALE t
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q16_mul t2 t1m
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-- ============================================================================
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-- Hermite spline evaluation
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-- ============================================================================
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/--
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H(t) = h00(t)·y₀ + h01(t)·y₁ + h10(t)·(h·m₀) − h11(t)·(h·m₁)
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The minus sign on h11·(h·m₁) compensates the algebraic sign of our `h11`
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definition relative to the conventional Hermite basis. Standard Hermite
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uses h11_std(t) = t²(t−1) = −t²(1−t) = −h11_code, so the formula is
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equivalent to the textbook Hermite interpolation polynomial.
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Returns the friction factor f as a Q16.16 value at normalized position t.
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-/
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def hermiteSpline (t : Int) : Int :=
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let h00_y0 := q16_mul (h00 t) Y0
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let h01_y1 := q16_mul (h01 t) Y1
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let h10_s0 := q16_mul (h10 t) H_M0
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let h11_s1 := q16_mul (h11 t) H_M1
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q16_add (q16_add h00_y0 h01_y1) (q16_sub h10_s0 h11_s1)
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/--
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Compute the friction factor f at a given Reynolds number.
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For Re < 2300: laminar (64/Re) approximated in Q16.16
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For 2300 ≤ Re ≤ 4000: Hermite spline bridge
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For Re > 4000: turbulent constant approximation
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Returns `none` for Re = 0 (division by zero in the laminar branch).
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-/
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def frictionFactor (re : Int) : Option Int :=
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if re < RE_LAMINAR then
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-- Laminar: f = 64/Re (Blasius laminar) in Q16.16: (64 * SCALE) / Re
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-- q16_div multiplies numerator by SCALE internally, so pass 64
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q16_div 64 re
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else if re > RE_TURBULENT then
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-- Turbulent: constant approximation at Re=4000
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some Y1
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else
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match normalizedT re with
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| some t => some (hermiteSpline t)
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| none => none
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-- ============================================================================
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-- Intermittency factor γ ∈ [0, SCALE] (Q16.16)
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-- γ = 0 fully laminar, γ = SCALE fully turbulent
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-- ============================================================================
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def intermittency (re : Int) : Option Int :=
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match normalizedT re with
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| none => none
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| some t =>
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let ft := hermiteSpline t
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let num := q16_sub ft Y0
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let den := q16_sub Y1 Y0
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q16_div num den
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-- ============================================================================
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-- Reynolds regime classification
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-- ============================================================================
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inductive Regime : Type
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| laminar
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| transitional
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| turbulent
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deriving Repr, DecidableEq
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def classifyRegime (re : Int) : Regime :=
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if re < RE_LAMINAR then .laminar
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else if re > RE_TURBULENT then .turbulent
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else .transitional
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-- ============================================================================
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-- 16D controller gate: maps Reynolds regime to controller action
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-- ============================================================================
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inductive GateAction : Type
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| admit
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| braid
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| refine
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| patch
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| loopback
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deriving Repr, DecidableEq
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def controllerGate (re : Int) : GateAction :=
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match classifyRegime re with
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| .laminar => .admit
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| .transitional => .braid
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| .turbulent => .patch
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-- ============================================================================
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-- Verification theorems (boundary conditions and correctness)
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-- ============================================================================
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-- Hermite boundary values ------------------------------------------------
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/-- The Hermite spline at t=0 equals Y0 (laminar boundary). -/
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theorem hermite_spline_at_zero : hermiteSpline 0 = Y0 := by
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native_decide
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/-- The Hermite spline at t=SCALE equals Y1 (turbulent boundary). -/
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theorem hermite_spline_at_one : hermiteSpline SCALE = Y1 := by
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native_decide
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-- Hermite basis function values at t=0 -----------------------------------
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theorem h00_at_zero : h00 0 = SCALE := by native_decide
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theorem h01_at_zero : h01 0 = 0 := by native_decide
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theorem h10_at_zero : h10 0 = 0 := by native_decide
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theorem h11_at_zero : h11 0 = 0 := by native_decide
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-- Hermite basis function values at t=SCALE (i.e. t=1) --------------------
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theorem h00_at_one : h00 SCALE = 0 := by native_decide
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theorem h01_at_one : h01 SCALE = SCALE := by native_decide
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theorem h10_at_one : h10 SCALE = 0 := by native_decide
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theorem h11_at_one : h11 SCALE = 0 := by native_decide
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-- Intermittency boundary values ------------------------------------------
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/-- `intermittency` returns `some` at the laminar exit. -/
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theorem intermittency_at_laminar_exit_some :
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(intermittency RE_LAMINAR).isSome := by
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native_decide
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/-- `intermittency` returns 0 at the laminar exit. -/
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theorem intermittency_at_laminar_exit :
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(intermittency RE_LAMINAR).get! = 0 := by
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native_decide
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/-- `intermittency` returns `some` at the turbulent entry. -/
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theorem intermittency_at_turbulent_entry_some :
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(intermittency RE_TURBULENT).isSome := by
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native_decide
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/-- Intermittency is SCALE at turbulent entry (fully turbulent). -/
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theorem intermittency_at_turbulent_entry :
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(intermittency RE_TURBULENT).get! = SCALE := by
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native_decide
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/-- Intermittency at the midpoint (Re=3150) is strictly between 0 and SCALE. -/
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theorem intermittency_midpoint_in_range :
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let v := (intermittency 3150).get!
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0 < v ∧ v < SCALE := by
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native_decide
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-- Friction factor boundary values ----------------------------------------
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/-- `frictionFactor` returns `some` at the laminar exit. -/
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theorem friction_at_laminar_exit_some :
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(frictionFactor RE_LAMINAR).isSome := by
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native_decide
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theorem friction_at_laminar_exit :
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(frictionFactor RE_LAMINAR).get! = Y0 := by
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native_decide
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/-- `frictionFactor` returns `some` at the turbulent entry. -/
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theorem friction_at_turbulent_entry_some :
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(frictionFactor RE_TURBULENT).isSome := by
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native_decide
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theorem friction_at_turbulent_entry :
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(frictionFactor RE_TURBULENT).get! = Y1 := by
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native_decide
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-- Regime classification --------------------------------------------------
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theorem laminar_classification : classifyRegime 1000 = Regime.laminar := by
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native_decide
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theorem transitional_classification : classifyRegime 3000 = Regime.transitional := by
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native_decide
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theorem turbulent_classification : classifyRegime 5000 = Regime.turbulent := by
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native_decide
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-- Controller gate --------------------------------------------------------
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theorem laminar_gate : controllerGate 1000 = GateAction.admit := by
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native_decide
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theorem transitional_gate : controllerGate 3000 = GateAction.braid := by
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native_decide
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theorem turbulent_gate : controllerGate 5000 = GateAction.patch := by
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native_decide
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-- ============================================================================
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-- Executable witnesses (computational receipts)
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-- ============================================================================
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#eval! Y0
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#eval! Y1
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#eval! hermiteSpline 0
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#eval! hermiteSpline SCALE
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#eval! (intermittency RE_LAMINAR).get!
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#eval! (intermittency RE_TURBULENT).get!
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#eval! (intermittency 3150).get!
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#eval! (frictionFactor 2300).get!
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#eval! (frictionFactor 4000).get!
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#eval! (frictionFactor 1000).get!
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end Semantics.Physics.UniversalBridge
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