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import OAI.MathematicalPhysics.Boltzmann.Approximation.CapActualLossDensity
import OAI.MathematicalPhysics.Boltzmann.Approximation.CapHotSourceIntegrability
import OAI.MathematicalPhysics.Boltzmann.Approximation.CapHotTransportBalance
import OAI.MathematicalPhysics.Boltzmann.Approximation.CapMixedCollisionLimits
import OAI.MathematicalPhysics.Boltzmann.Approximation.CapNonlinearHotLimit
import OAI.MathematicalPhysics.Boltzmann.Branching.CentralRetainedLimit
import OAI.MathematicalPhysics.Boltzmann.Branching.CharacteristicPhysicalGain
import OAI.MathematicalPhysics.Boltzmann.Branching.CharacteristicProductTest
import OAI.MathematicalPhysics.Boltzmann.Branching.HotChartHomeomorph
import OAI.MathematicalPhysics.Boltzmann.Branching.HotPositiveRegion
import OAI.MathematicalPhysics.Boltzmann.Branching.IncomingLossRate
import OAI.MathematicalPhysics.Boltzmann.Branching.MixedPhysicalMeasures
import OAI.MathematicalPhysics.Boltzmann.Branching.ProjectedTimeBalance
import OAI.MathematicalPhysics.Boltzmann.Branching.SeparatedMeasureTail
import OAI.MathematicalPhysics.Boltzmann.Branching.VanishingCutoffCollision
import OAI.MathematicalPhysics.Boltzmann.Collision.CollisionSources
import OAI.MathematicalPhysics.Boltzmann.Jets.ColdCentralVanishing
namespace OAI
section
/-! # The physical hot collision decomposition on each compact time cylinder -/
noncomputable section
open MeasureTheory Filter Set
open scoped Topology ENNReal
open BoltzmannNonuniqueness.VelocityWeight BoltzmannNonuniqueness.CollisionCompactness
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
theorem eventually_hot_collision_identity (hcarleman : Published.GPV2009CarlemanInput)
(S : AttainedCapSequence F)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hd₀ : 0 ≤ d₀) (hq₁ : 1 < q) (hq₂ : q < 2)
{κ : ℕ → ℕ} {U : ℝ≥0∞}
(hU : Tendsto (fun n => S.normalizedHorizon (κ n)) atTop (𝓝 U))
{a A R : ℝ} (ha : 0 ≤ a) (hA : ENNReal.ofReal A < U) :
∀ᶠ n in atTop, ∀ᵐ z ∂(coldCylinderVolume a A R).prod volume,
S.hotSourceDensity a A (κ n) z =
2*mixedGainDensity (F.indices (κ n)+1) (S.rescaledColdDensity (κ n)) (S.hotDensity (κ n)) z-
S.hotDensity (κ n) z*KineticCollisionNullSets.frequency (F.indices (κ n)+1)
(S.rescaledColdDensity (κ n)) z+
(S.radius (κ n))^2*collisionSource (F.indices (κ n)+1) (S.hotDensity (κ n)) z+
H q z.2*S.rescaledColdSource (κ n) (z.1.1,(z.1.2,z.2)) := by
filter_upwards [S.eventually_extendedHot_eq hs₀ hU hA] with n hn
have ht : ∀ᵐ z ∂(coldCylinderVolume a A R).prod (volume : Measure Velocity),
z.1.1 ∈ Icc a A :=
Measure.quasiMeasurePreserving_fst.ae
(Measure.quasiMeasurePreserving_fst.ae (ae_restrict_mem measurableSet_Icc))
have hg : ∀ᵐ z ∂(coldCylinderVolume a A R).prod (volume : Measure Velocity),
z.2 ∈ HotRepresentative.good q :=
Measure.quasiMeasurePreserving_snd.ae (HotRepresentative.ae_good hcarleman hq₁ hq₂)
filter_upwards [ht,hg] with z hz hzg
have he (v : Velocity) : S.hotDensity (κ n) (z.1,v) = S.physicalHotDensity (κ n) (z.1,v) :=
hn z.1.1 ⟨ha.trans hz.1,hz.2⟩ (z.1.2,v)
have hi := S.rescaled_hot_collision hs₀ hsmax hη hηmax hK hd₀ hq₂ (κ n) z hzg
rw [mixedGain_fiber_congr _ (fun _ => rfl) (fun v => (he v).symm) z.2,
collisionSource_fiber_congr _ (fun v => (he v).symm) z.2,← he z.2] at hi
rw [hotSourceDensity,indicator_of_mem
(show z ∈ {z : HotKineticPhase | z.1.1 ∈ Icc a A} from hz)]
exact hi
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # General compact kinetic tests for the actual loss measure limit -/
noncomputable section
open MeasureTheory Set Filter
open scoped ENNReal Topology BoundedContinuousFunction
open BoltzmannNonuniqueness.CollisionCompactness
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotPairExtraction.loss_measure_compact_limit
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2) {a A R : ℝ}
(ha : 0 < a) (haA : a ≤ A) (hA : ENNReal.ofReal A < E.horizon) (hR : 0 ≤ R)
(ψ : C(HotKineticPhase,ℝ)) (hc : HasCompactSupport ψ) :
Tendsto (fun n => ∫ z, ψ z ∂S.physicalLossMeasure a A R (E.indices n)) atTop
(𝓝 (∫ z, ψ z ∂incomingLossMeasure
(E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) := by
let ν := incomingLossMeasure
(E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))
let _ : IsFiniteMeasure ν :=
E.toHotLimitExtraction.incomingLossMeasure_finite ha (ha.le.trans haA) hK hα hγ hq₂
have hfin := (S.eventually_physicalCollisionMeasures_finite hs₀ hsmax hη hηmax hK hα
(hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₂ E.indices_strict E.horizon_limit
(R := R) ha haA hA).mono (fun _ hn => hn.2)
have hsep (u : (ℝ × JetPrototype.Space) →ᵇ ℝ) (v : Velocity →ᵇ ℝ) :
Tendsto (fun n => ∫ z, u z.1*v z.2 ∂S.physicalLossMeasure a A R (E.indices n)) atTop
(𝓝 (∫ z, u z.1*v z.2 ∂ν)) :=
E.loss_measure_separated_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ
hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR u.continuous.measurable
(fun x => u.norm_coe_le_norm x) v.continuous (fun x => v.norm_coe_le_norm x)
obtain ⟨RX,hRX⟩ := (hc.isCompact.image continuous_fst).isBounded.subset_closedBall
(0 : ℝ × JetPrototype.Space)
obtain ⟨RV,hRV⟩ := (hc.isCompact.image continuous_snd).isBounded.subset_closedBall (0 : Velocity)
apply SeparatedTests.compact_test_tendsto_of_eventually_finite _ ν hfin hsep ψ hc 0 0 RX RV
intro z hz
apply image_eq_zero_of_notMem_tsupport
intro hzs
exact hz ⟨hRX ⟨z,hzs,rfl⟩,hRV ⟨z,hzs,rfl⟩⟩
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # Source identity with exactly the physical error controlled by compactness -/
noncomputable section
open MeasureTheory Filter Set
open scoped Topology ENNReal
open BoltzmannNonuniqueness.CollisionCompactness
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
theorem eventually_hot_source_error_identity (hcarleman : Published.GPV2009CarlemanInput)
(S : AttainedCapSequence F)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hd₀ : 0 ≤ d₀) (hq₁ : 1 < q) (hq₂ : q < 2)
{κ : ℕ → ℕ} {U : ℝ≥0∞}
(hU : Tendsto (fun n => S.normalizedHorizon (κ n)) atTop (𝓝 U))
{a A R : ℝ} (ha : 0 ≤ a) (hA : ENNReal.ofReal A < U) :
∀ᶠ n in atTop, ∀ᵐ z ∂(coldCylinderVolume a A R).prod volume,
S.hotSourceDensity a A (κ n) z =
2*mixedGainDensity (F.indices (κ n)+1) (S.rescaledColdDensity (κ n)) (S.hotDensity (κ n)) z-
S.hotDensity (κ n) z*KineticCollisionNullSets.frequency (F.indices (κ n)+1)
(S.rescaledColdDensity (κ n)) z+S.physicalCollisionError a A (κ n) z := by
filter_upwards [S.eventually_hot_collision_identity hcarleman hs₀ hsmax hη hηmax hK hd₀
hq₁ hq₂ hU (R := R) ha hA,S.eventually_extendedHot_eq hs₀ hU hA] with n hn hext
have ht : ∀ᵐ z ∂(coldCylinderVolume a A R).prod (volume : Measure Velocity),
z.1.1 ∈ Icc a A :=
Measure.quasiMeasurePreserving_fst.ae
(Measure.quasiMeasurePreserving_fst.ae (ae_restrict_mem measurableSet_Icc))
filter_upwards [hn,ht] with z hz hzt
have he (v : Velocity) : S.hotDensity (κ n) (z.1,v) = S.physicalHotDensity (κ n) (z.1,v) :=
hext z.1.1 ⟨ha.trans hzt.1,hzt.2⟩ (z.1.2,v)
rw [collisionSource_fiber_congr _ he z.2] at hz
unfold physicalCollisionError coldSourceDensity
rw [indicator_of_mem (show z ∈ {z : HotKineticPhase | z.1.1 ∈ Icc a A} from hzt)]
simpa only [add_assoc] using hz
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # Identification of the actual rescaled hot source against separated tests -/
noncomputable section
open MeasureTheory Filter
open scoped Topology ENNReal
open BoltzmannNonuniqueness.CollisionCompactness
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotPairExtraction.hot_source_weak_limit
(hDP : Published.DunfordPettis1940HotPairWindows)
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2) :
∃ κ : ℕ → ℕ, StrictMono κ ∧ ∀ a A R : ℝ, ∀ ha : 0 < a, a ≤ A →
ENNReal.ofReal A < E.horizon → 0 ≤ R →
∀ (θ : ℝ × JetPrototype.Space → ℝ), Measurable θ →
∀ B : ℝ, (∀ x, |θ x| ≤ B) →
∀ (φ : Velocity → ℝ), Continuous φ → ∀ C : ℝ, (∀ v, |φ v| ≤ C) →
Tendsto (fun n => ∫ z, (θ z.1*φ z.2)*S.hotSourceDensity a A (E.indices (κ n)) z
∂(coldCylinderVolume a A R).prod volume) atTop
(𝓝 (2*(∫ z, θ z.1*incomingGainTest φ z.2
∂E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))-
(∫ z, θ z.1*incomingLossTest φ z.2
∂E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) := by
obtain ⟨κ,hκ,herr⟩ := E.vanishing_physical_collision_error hDP hcarleman hGLPS hs₀ hsmax hη hηmax
hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₁ hq₂
refine ⟨κ,hκ,fun a A R ha haA hA hR θ hθ B hθB φ hφ C hφC => ?_⟩
let ψ : HotKineticPhase → ℝ := fun z => θ z.1*φ z.2
have hψ : Measurable ψ := (hθ.comp measurable_fst).mul (hφ.measurable.comp measurable_snd)
have hB : 0 ≤ B := (abs_nonneg (θ (0,0))).trans (hθB _)
have hC : 0 ≤ C := (abs_nonneg (φ 0)).trans (hφC _)
have hψB (z) : |ψ z| ≤ B*C := by
exact (abs_mul _ _).trans_le (mul_le_mul (hθB _) (hφC _) (abs_nonneg _) hB)
have he := Compactness.bounded_test_integral_tendsto_zero
(fun n => (S.physicalCollisionError_measurable hs₀ hsmax hη hηmax hK hd₀.le hq₂ a A
(E.indices (κ n))).aestronglyMeasurable)
(herr a A R ha haA hA) hψ (mul_nonneg hB hC) hψB
have hg := (E.mixed_physical_gain_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ
hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR hθ hθB hφ hφC).comp hκ.tendsto_atTop
have hl := (E.mixed_physical_loss_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ
hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR hθ hθB hφ hφC).comp hκ.tendsto_atTop
have ht := ((hg.const_mul 2).sub hl).add he
simp only [add_zero] at ht
apply ht.congr'
have hei : ∀ᶠ n in atTop, Integrable (S.physicalCollisionError a A (E.indices (κ n)))
((coldCylinderVolume a A R).prod volume) :=
((herr a A R ha haA hA).eventually
(eventually_lt_nhds (show (0 : ℝ≥0∞) < ⊤ from ENNReal.coe_lt_top))).mono
(fun _ hn => memLp_one_iff_integrable.mp hn)
filter_upwards [S.eventually_hot_source_error_identity hcarleman hs₀ hsmax hη hηmax hK
hd₀.le hq₁ hq₂ (E.horizon_limit.comp hκ.tendsto_atTop) (R := R) ha.le hA,
S.eventually_mixedPreRate_integrable hs₀ hsmax hη hηmax hK hα
(hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₂ (E.indices_strict.comp hκ)
(E.horizon_limit.comp hκ.tendsto_atTop) (R := R) ha haA hA,hei] with n hn hpre hei
have hp := hpre (S.collisionCutoff (E.indices (κ n)))
have hgi := mixed_gain_test_integrable hp hψ hψB
have hli := mixed_loss_test_integrable hp hψ hψB
have heψ := hei.bdd_mul hψ.aestronglyMeasurable (ae_of_all _ hψB)
dsimp only [Function.comp_def,ψ] at hgi hli heψ ⊢
have hsum := integral_add ((hgi.const_mul 2).sub hli) heψ
simp only [Pi.sub_apply] at hsum
rw [← integral_const_mul,← integral_sub (hgi.const_mul 2) hli,← hsum]
apply integral_congr_ae
filter_upwards [hn] with z hz
rw [hz]
change _ = (θ z.1*φ z.2)*(2*mixedGainDensity (S.collisionCutoff (E.indices (κ n)))
(S.rescaledColdDensity (E.indices (κ n))) (S.hotDensity (E.indices (κ n))) z-
S.hotDensity (E.indices (κ n)) z*KineticCollisionNullSets.frequency
(S.collisionCutoff (E.indices (κ n))) (S.rescaledColdDensity (E.indices (κ n))) z+
S.physicalCollisionError a A (E.indices (κ n)) z)
ring
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # Separated-test convergence of the actual physical gain measures -/
noncomputable section
open MeasureTheory Set Filter
open scoped ENNReal Topology
open BoltzmannNonuniqueness.CollisionCompactness
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotPairExtraction.gain_measure_separated_limit
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2) {a A R : ℝ}
(ha : 0 < a) (haA : a ≤ A) (hA : ENNReal.ofReal A < E.horizon) (hR : 0 ≤ R)
{B : ℝ} {θ : ℝ × JetPrototype.Space → ℝ} (hθ : Measurable θ) (hθB : ∀ x, |θ x| ≤ B)
{φ : Velocity → ℝ} (hφ : Continuous φ) {C : ℝ} (hφC : ∀ v, |φ v| ≤ C) :
Tendsto (fun n => ∫ z, θ z.1*φ z.2 ∂S.physicalGainMeasure a A R (E.indices n)) atTop
(𝓝 (∫ z, θ z.1*φ z.2 ∂incomingGainMeasure
(E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) := by
let μ := E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)
let _ : SFinite μ := by dsimp [μ,HotLimitExtraction.mixedMeasure]; infer_instance
have hi : Integrable incomingRate μ :=
E.toHotLimitExtraction.incomingRate_integrable ha (ha.le.trans haA) hK hα hγ hq₂
have hB : 0 ≤ B := (abs_nonneg (θ (0,0))).trans (hθB _)
have ht := E.mixed_physical_gain_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax
hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR hθ hθB hφ hφC
rw [← incomingGainMeasure_separated hi hθ hB hθB hφ.measurable hφC] at ht
apply ht.congr'
filter_upwards [S.eventually_mixedPreRate_integrable hs₀ hsmax hη hηmax hK hα
(hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₂ E.indices_strict E.horizon_limit
(R := R) ha haA hA] with n hn
have hc := fun p => (S.rescaledColdDensity_bounds hs₀ hsmax hη hηmax hK hd₀.le hq₂ (E.indices n) p).1
have hh := S.hotDensity_nonneg hs₀ hsmax hη hηmax hK hd₀.le hq₂ (E.indices n)
exact (mixedGainMeasure_integral hc hh (hn _) (fun z => θ z.1*φ z.2)).symm
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # General compact kinetic tests for the actual gain measure limit -/
noncomputable section
open MeasureTheory Set Filter
open scoped ENNReal Topology BoundedContinuousFunction
open BoltzmannNonuniqueness.CollisionCompactness
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotPairExtraction.gain_measure_compact_limit
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2) {a A R : ℝ}
(ha : 0 < a) (haA : a ≤ A) (hA : ENNReal.ofReal A < E.horizon) (hR : 0 ≤ R)
(ψ : C(HotKineticPhase,ℝ)) (hc : HasCompactSupport ψ) :
Tendsto (fun n => ∫ z, ψ z ∂S.physicalGainMeasure a A R (E.indices n)) atTop
(𝓝 (∫ z, ψ z ∂incomingGainMeasure
(E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) := by
let ν := incomingGainMeasure
(E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))
let _ : IsFiniteMeasure ν :=
E.toHotLimitExtraction.incomingGainMeasure_finite ha (ha.le.trans haA) hK hα hγ hq₂
have hfin := (S.eventually_physicalCollisionMeasures_finite hs₀ hsmax hη hηmax hK hα
(hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₂ E.indices_strict E.horizon_limit
(R := R) ha haA hA).mono (fun _ hn => hn.1)
have hsep (u : (ℝ × JetPrototype.Space) →ᵇ ℝ) (v : Velocity →ᵇ ℝ) :
Tendsto (fun n => ∫ z, u z.1*v z.2 ∂S.physicalGainMeasure a A R (E.indices n)) atTop
(𝓝 (∫ z, u z.1*v z.2 ∂ν)) :=
E.gain_measure_separated_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ
hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR u.continuous.measurable
(fun x => u.norm_coe_le_norm x) v.continuous (fun x => v.norm_coe_le_norm x)
obtain ⟨RX,hRX⟩ := (hc.isCompact.image continuous_fst).isBounded.subset_closedBall
(0 : ℝ × JetPrototype.Space)
obtain ⟨RV,hRV⟩ := (hc.isCompact.image continuous_snd).isBounded.subset_closedBall (0 : Velocity)
apply SeparatedTests.compact_test_tendsto_of_eventually_finite _ ν hfin hsep ψ hc 0 0 RX RV
intro z hz
apply image_eq_zero_of_notMem_tsupport
intro hzs
exact hz ⟨hRX ⟨z,hzs,rfl⟩,hRV ⟨z,hzs,rfl⟩⟩
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # The linear hot transport equation for the actual extracted cap limit
Mixed cold-hot convergence identifies the collision source. Compactness and
Carleman hypotheses give the linear transport equation for the extracted limit.
-/
noncomputable section
open MeasureTheory Filter Set
open scoped Topology ENNReal
open BoltzmannNonuniqueness.TransportCutoff BoltzmannNonuniqueness.CollisionCompactness
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotPairExtraction.separated_transport_balance
(hDP : Published.DunfordPettis1940HotPairWindows)
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2)
{a A B R Rₑ : ℝ} (ha : 0 < a) (haA : a ≤ A) (hAB : A < B)
(hB : ENNReal.ofReal B < E.horizon) (hR : 0 ≤ R)
{χ : Published.KineticPhase → ℝ} (hχ : ContDiff ℝ (⊤ : ℕ∞) χ)
(hc : HasCompactSupport χ) (hs : tsupport χ ⊆ kineticWindow a A Rₑ)
(hsC : ∀ z ∈ tsupport χ, EuclideanFlight.hotChart z ∈ coldCylinderSet a A R)
{θ : ℝ × JetPrototype.Space → ℝ} (hθ : Measurable θ)
{Cθ : ℝ} (hθB : ∀ x, |θ x| ≤ Cθ)
{φ : Velocity → ℝ} (hφ : Continuous φ) {Cφ : ℝ} (hφB : ∀ v, |φ v| ≤ Cφ)
(hsep : ∀ z, χ (EuclideanFlight.hotChart.symm z) = θ z.1*φ z.2) :
(∫ z, transportDerivative χ (EuclideanFlight.hotChart.symm z)*E.hotLimit z
∂(coldCylinderVolume a A R).prod volume) +
(2*(∫ z, θ z.1*incomingGainTest φ z.2
∂E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))-
(∫ z, θ z.1*incomingLossTest φ z.2
∂E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) = 0 := by
have hA : ENNReal.ofReal A < E.horizon :=
(ENNReal.ofReal_le_ofReal hAB.le).trans_lt hB
obtain ⟨κ,hκ,hsource⟩ := E.hot_source_weak_limit hDP hcarleman hGLPS hs₀ hsmax hη hηmax
hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂
let μ := (coldCylinderVolume a A R).prod (volume : Measure Velocity)
let D : HotKineticPhase → ℝ := fun z => transportDerivative χ (EuclideanFlight.hotChart.symm z)
have hDm : Measurable D :=
(transportDerivative_continuous hχ).measurable.comp EuclideanFlight.hotChart.symm.measurable
obtain ⟨CD,hDb⟩ := (transportDerivative_continuous hχ).bounded_above_of_compact_support
(transportDerivative_hasCompactSupport hc)
have hDB (z) : |D z| ≤ CD := hDb _
have hlimF := ((E.toHotLimitExtraction.physical_weak_cylinder S hs₀ ha.le hA R).2.2
D hDm ⟨CD,hDB⟩).comp hκ.tendsto_atTop
have hlimQ := hsource a A R ha haA hA hR θ hθ Cθ hθB φ hφ Cφ hφB
have hlim := hlimF.add hlimQ
have hψ : Measurable (fun z : HotKineticPhase => θ z.1*φ z.2) :=
(hθ.comp measurable_fst).mul (hφ.measurable.comp measurable_snd)
have hCθ : 0 ≤ Cθ := (abs_nonneg (θ (0,0))).trans (hθB _)
have hψB (z : HotKineticPhase) : |θ z.1*φ z.2| ≤ Cθ*Cφ := by
rw [abs_mul]
exact mul_le_mul (hθB _) (hφB _) (abs_nonneg _) hCθ
have he : (fun n => (∫ z, D z*S.physicalHotDensity (E.indices (κ n)) z ∂μ)+
(∫ z, (θ z.1*φ z.2)*S.hotSourceDensity a A (E.indices (κ n)) z ∂μ)) =ᶠ[atTop]
(fun _ => (0 : ℝ)) := by
filter_upwards [hκ.tendsto_atTop.eventually
(S.eventually_physicalHot_cylinder_integrable E.toHotLimitExtraction hs₀
hsmax hη hηmax hK hd₀.le hq₂ ha.le hA R),
S.eventually_hotSource_cylinder_integrable hcarleman hs₀ hsmax hη hηmax hK hα
(hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₁ hq₂
(E.indices_strict.comp hκ) (E.horizon_limit.comp hκ.tendsto_atTop) ha haA hA R,
S.eventually_hot_transport_balance hcarleman hs₀ hsmax hη hηmax hK hα
(hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₁ hq₂
(E.indices_strict.comp hκ) (E.horizon_limit.comp hκ.tendsto_atTop)
ha haA hAB hB hχ hc hs] with n hfi hqi hbal
have hiF := hfi.bdd_mul hDm.aestronglyMeasurable (ae_of_all _ hDB)
have hiQ := hqi.bdd_mul hψ.aestronglyMeasurable (ae_of_all _ hψB)
dsimp only [μ,Function.comp_def] at hiQ ⊢
rw [← integral_add hiF hiQ]
have hb := S.hot_transport_cylinder_of_balance (E.indices (κ n)) hsC hbal
simpa only [D,μ,hsep] using hb
exact tendsto_nhds_unique hlim (tendsto_const_nhds.congr' he.symm)
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # The actual hot source limit for every compact continuous kinetic test -/
noncomputable section
open MeasureTheory Filter
open scoped Topology ENNReal
open BoltzmannNonuniqueness.CollisionCompactness
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotPairExtraction.hot_source_compact_limit
(hDP : Published.DunfordPettis1940HotPairWindows)
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2) :
∃ κ : ℕ → ℕ, StrictMono κ ∧ ∀ a A R : ℝ, ∀ ha : 0 < a, a ≤ A →
ENNReal.ofReal A < E.horizon → 0 ≤ R →
∀ ψ : C(HotKineticPhase,ℝ), HasCompactSupport ψ →
Tendsto (fun n => ∫ z, ψ z*S.hotSourceDensity a A (E.indices (κ n)) z
∂(coldCylinderVolume a A R).prod volume) atTop
(𝓝 (2*(∫ z, ψ z ∂incomingGainMeasure
(E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))-
(∫ z, ψ z ∂incomingLossMeasure
(E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))))) := by
obtain ⟨κ,hκ,herr⟩ := E.vanishing_physical_collision_error hDP hcarleman hGLPS hs₀ hsmax hη hηmax
hK hα (hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₁ hq₂
refine ⟨κ,hκ,fun a A R ha haA hA hR ψ hc => ?_⟩
obtain ⟨B,hB⟩ := ψ.continuous.bounded_above_of_compact_support hc
have hB0 : 0 ≤ B := (abs_nonneg (ψ 0)).trans (hB _)
have he := Compactness.bounded_test_integral_tendsto_zero
(fun n => (S.physicalCollisionError_measurable hs₀ hsmax hη hηmax hK hd₀.le hq₂ a A
(E.indices (κ n))).aestronglyMeasurable)
(herr a A R ha haA hA) ψ.continuous.measurable hB0 hB
have hg := (E.gain_measure_compact_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ
hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR ψ hc).comp hκ.tendsto_atTop
have hl := (E.loss_measure_compact_limit hcarleman hGLPS hs₀ hsmax hη hηmax hK hα hαmax hγ
hd₀ hd₀max hsmall hq₁ hq₂ ha haA hA hR ψ hc).comp hκ.tendsto_atTop
have ht := ((hg.const_mul 2).sub hl).add he
simp only [add_zero] at ht
apply ht.congr'
have hei : ∀ᶠ n in atTop, Integrable (S.physicalCollisionError a A (E.indices (κ n)))
((coldCylinderVolume a A R).prod volume) :=
((herr a A R ha haA hA).eventually
(eventually_lt_nhds (show (0 : ℝ≥0∞) < ⊤ from ENNReal.coe_lt_top))).mono
(fun _ hn => memLp_one_iff_integrable.mp hn)
filter_upwards [S.eventually_hot_source_error_identity hcarleman hs₀ hsmax hη hηmax hK
hd₀.le hq₁ hq₂ (E.horizon_limit.comp hκ.tendsto_atTop) (R := R) ha.le hA,
S.eventually_mixedPreRate_integrable hs₀ hsmax hη hηmax hK hα
(hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₂ (E.indices_strict.comp hκ)
(E.horizon_limit.comp hκ.tendsto_atTop) (R := R) ha haA hA,hei] with n hn hpre hei
dsimp only [Function.comp_def] at hpre
have hp := hpre (S.collisionCutoff (E.indices (κ n)))
have hcold := fun p => (S.rescaledColdDensity_bounds hs₀ hsmax hη hηmax hK hd₀.le hq₂
(E.indices (κ n)) p).1
have hhot := S.hotDensity_nonneg hs₀ hsmax hη hηmax hK hd₀.le hq₂ (E.indices (κ n))
have hgi := mixed_gain_test_integrable hp ψ.continuous.measurable hB
have hli := (mixedLossDensity_integrable hp).bdd_mul ψ.continuous.aestronglyMeasurable
(ae_of_all _ hB)
have heψ := hei.bdd_mul ψ.continuous.aestronglyMeasurable (ae_of_all _ hB)
dsimp only [Function.comp_def,physicalGainMeasure,physicalLossMeasure]
rw [mixedGainMeasure_integral hcold hhot hp ψ,mixedLossMeasure_integral hcold hhot hp ψ,
← integral_const_mul,← integral_sub (hgi.const_mul 2) hli]
have hsub := (hgi.const_mul 2).sub hli
change Integrable (fun z => (2 : ℝ)*(ψ z*_) - ψ z*_) _ at hsub
rw [← integral_add hsub heψ]
apply integral_congr_ae
filter_upwards [hn,mixed_loss_ae_eq_frequency hp] with z hz hlz
rw [hz,hlz]
change _ = ψ z*(2*mixedGainDensity (S.collisionCutoff (E.indices (κ n)))
(S.rescaledColdDensity (E.indices (κ n))) (S.hotDensity (E.indices (κ n))) z-
S.hotDensity (E.indices (κ n)) z*KineticCollisionNullSets.frequency
(S.collisionCutoff (E.indices (κ n))) (S.rescaledColdDensity (E.indices (κ n))) z+
S.physicalCollisionError a A (E.indices (κ n)) z)
ring
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # The actual limiting hot equation for every smooth compact kinetic test
Mixed cold-hot convergence identifies the collision source. Compactness and
Carleman hypotheses give the transport equation for the extracted limit.
-/
noncomputable section
open MeasureTheory Filter Set
open scoped Topology ENNReal
open BoltzmannNonuniqueness.TransportCutoff BoltzmannNonuniqueness.CollisionCompactness
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotPairExtraction.transport_measure_balance
(hDP : Published.DunfordPettis1940HotPairWindows)
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2)
{a A B R Rₑ : ℝ} (ha : 0 < a) (haA : a ≤ A) (hAB : A < B)
(hB : ENNReal.ofReal B < E.horizon) (hR : 0 ≤ R)
{χ : Published.KineticPhase → ℝ} (hχ : ContDiff ℝ (⊤ : ℕ∞) χ)
(hc : HasCompactSupport χ) (hs : tsupport χ ⊆ kineticWindow a A Rₑ)
(hsC : ∀ z ∈ tsupport χ, EuclideanFlight.hotChart z ∈ coldCylinderSet a A R)
:
(∫ z, transportDerivative χ (EuclideanFlight.hotChart.symm z)*E.hotLimit z
∂(coldCylinderVolume a A R).prod volume) +
(2*(∫ z, χ (EuclideanFlight.hotChart.symm z) ∂incomingGainMeasure
(E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))-
(∫ z, χ (EuclideanFlight.hotChart.symm z) ∂incomingLossMeasure
(E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) = 0 := by
have hA : ENNReal.ofReal A < E.horizon :=
(ENNReal.ofReal_le_ofReal hAB.le).trans_lt hB
obtain ⟨κ,hκ,hsource⟩ := E.hot_source_compact_limit hDP hcarleman hGLPS hs₀ hsmax hη hηmax
hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂
let μ := (coldCylinderVolume a A R).prod (volume : Measure Velocity)
let D : HotKineticPhase → ℝ := fun z => transportDerivative χ (EuclideanFlight.hotChart.symm z)
have hDm : Measurable D :=
(transportDerivative_continuous hχ).measurable.comp EuclideanFlight.hotChart.symm.measurable
obtain ⟨CD,hDb⟩ := (transportDerivative_continuous hχ).bounded_above_of_compact_support
(transportDerivative_hasCompactSupport hc)
have hDB (z) : |D z| ≤ CD := hDb _
have hlimF := ((E.toHotLimitExtraction.physical_weak_cylinder S hs₀ ha.le hA R).2.2
D hDm ⟨CD,hDB⟩).comp hκ.tendsto_atTop
let ψ : C(HotKineticPhase,ℝ) := ⟨fun z => χ (EuclideanFlight.hotChart.symm z),
hχ.continuous.comp EuclideanFlight.hotChart_symm_continuous⟩
have hlimQ := hsource a A R ha haA hA hR ψ (EuclideanFlight.compact_test_hotChart hc)
have hlim := hlimF.add hlimQ
obtain ⟨Cψ,hψB⟩ := ψ.continuous.bounded_above_of_compact_support
(EuclideanFlight.compact_test_hotChart hc)
have he : (fun n => (∫ z, D z*S.physicalHotDensity (E.indices (κ n)) z ∂μ)+
(∫ z, ψ z*S.hotSourceDensity a A (E.indices (κ n)) z ∂μ)) =ᶠ[atTop]
(fun _ => (0 : ℝ)) := by
filter_upwards [hκ.tendsto_atTop.eventually
(S.eventually_physicalHot_cylinder_integrable E.toHotLimitExtraction hs₀
hsmax hη hηmax hK hd₀.le hq₂ ha.le hA R),
S.eventually_hotSource_cylinder_integrable hcarleman hs₀ hsmax hη hηmax hK hα
(hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₁ hq₂
(E.indices_strict.comp hκ) (E.horizon_limit.comp hκ.tendsto_atTop) ha haA hA R,
S.eventually_hot_transport_balance hcarleman hs₀ hsmax hη hηmax hK hα
(hαmax.trans (by norm_num)) hγ hd₀ hd₀max hsmall hq₁ hq₂
(E.indices_strict.comp hκ) (E.horizon_limit.comp hκ.tendsto_atTop)
ha haA hAB hB hχ hc hs] with n hfi hqi hbal
have hiF := hfi.bdd_mul hDm.aestronglyMeasurable (ae_of_all _ hDB)
have hiQ := hqi.bdd_mul ψ.continuous.aestronglyMeasurable (ae_of_all _ hψB)
dsimp only [μ,Function.comp_def] at hiQ ⊢
rw [← integral_add hiF hiQ]
have hb := S.hot_transport_cylinder_of_balance (E.indices (κ n)) hsC hbal
simpa only [D,μ,ψ,ContinuousMap.coe_mk] using hb
exact tendsto_nhds_unique hlim (tendsto_const_nhds.congr' he.symm)
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # Exact periodicity of the cap hot remainder and its bounded ratio -/
noncomputable section
open MeasureTheory
open BoltzmannNonuniqueness.WeightedTranslation BoltzmannNonuniqueness.WeightedLocal
open BoltzmannNonuniqueness.WeightedLocalControl BoltzmannNonuniqueness.VelocityWeight
namespace BoltzmannNonuniqueness.JetCopyDatum
theorem CapApproximation.hot_periodic {s₀ η K α γ d₀ q T : ℝ} {N : ℕ}
(F : CapApproximation s₀ η K α γ d₀ q T N) (k : JetLattice.Lattice) :
pull (displacement k) F.hot = F.hot := by
funext u
change F.solution.value (u.1,shift (displacement k) u.2)-
(∑' i, rebuilt s₀ η K α γ d₀ q (N+1) (damping q (N+1) F.amplitude) T N
F.solution.value i (u.1,shift (displacement k) u.2)) = _
have hs := congrFun (F.solution.periodic k) u
have hc (i : JetLattice.Label) := congrFun (rebuilt_shift
(s₀ := s₀) (η := η) (K := K) (α := α) (γ := γ) (d₀ := d₀) (q := q)
(b := N+1) (L := damping q (N+1) F.amplitude) (T := T) (N := N)
k (F.solution.periodic k) i) u
change F.solution.value (u.1,shift (displacement k) u.2) = F.solution.value u at hs
simp only [pull] at hc
rw [hs]
simp_rw [hc]
exact congrArg (fun c => F.solution.value u-c)
((relabel k).tsum_eq (fun i => rebuilt s₀ η K α γ d₀ q (N+1)
(damping q (N+1) F.amplitude) T N F.solution.value i u))
namespace AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
theorem euclideanHot_div_weight (S : AttainedCapSequence F) (n : ℕ) (z : Published.KineticPhase) :
S.euclideanHot n z/H q z.2 = (F.approximation n).hot
(S.radius n*z.1.1,(S.radius n • JetPeriodicDatum.spatialMap z.1.2,z.2))/S.radius n := by
rw [euclideanHot_eq_rescaledHot,rescaledHot_eq_weighted]
simp only [EuclideanFlight.phaseEquiv_apply,JetPeriodicDatum.phaseMap]
rw [mul_div_cancel_left₀ _ (H_pos q z.2).ne']
rfl
theorem boundedHotRatio_periodic (S : AttainedCapSequence F) (hs₀ : 0 < s₀)
(n : ℕ) (t : ℝ) (k : JetLattice.Lattice) (p : Velocity × Velocity) :
S.boundedHotRatio n ((t,p.1-(S.radius n)⁻¹ • latticeVector k),p.2) =
S.boundedHotRatio n ((t,p.1),p.2) := by
unfold boundedHotRatio
rw [euclideanHot_div_weight,euclideanHot_div_weight]
have he : S.radius n • JetPeriodicDatum.spatialMap (p.1-(S.radius n)⁻¹ • latticeVector k) =
S.radius n • JetPeriodicDatum.spatialMap p.1-displacement k := by
apply Prod.ext
· ext i
change S.radius n*(p.1 i.castSucc-(S.radius n)⁻¹*(k i.castSucc:ℝ)) =
S.radius n*p.1 i.castSucc-(k i.castSucc:ℝ)
field_simp [(S.radius_pos hs₀ n).ne']
· change S.radius n*(p.1 (Fin.last 2)-(S.radius n)⁻¹*(k (Fin.last 2):ℝ)) =
S.radius n*p.1 (Fin.last 2)-(k (Fin.last 2):ℝ)
field_simp [(S.radius_pos hs₀ n).ne']
rw [he]
have hp := congrFun ((F.approximation n).hot_periodic k)
(S.radius n*t,(S.radius n • JetPeriodicDatum.spatialMap p.1,p.2))
change (F.approximation n).hot
(S.radius n*t,(S.radius n • JetPeriodicDatum.spatialMap p.1-displacement k,p.2)) = _ at hp
rw [hp]
end AttainedCapSequence
end BoltzmannNonuniqueness.JetCopyDatum
end
end
section
/-! # The actual limiting transport equation with its loss attenuation -/
noncomputable section
open MeasureTheory Set
open scoped ENNReal
open BoltzmannNonuniqueness.TransportCutoff BoltzmannNonuniqueness.CollisionCompactness
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotPairExtraction.attenuated_transport_balance
(hDP : Published.DunfordPettis1940HotPairWindows)
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2)
{a A B R Rₑ : ℝ} (ha : 0 < a) (haA : a ≤ A) (hAB : A < B)
(hB : ENNReal.ofReal B < E.horizon) (hR : 0 ≤ R)
{χ : Published.KineticPhase → ℝ} (hχ : ContDiff ℝ (⊤ : ℕ∞) χ)
(hc : HasCompactSupport χ) (hs : tsupport χ ⊆ kineticWindow a A Rₑ)
(hsC : ∀ z ∈ tsupport χ, EuclideanFlight.hotChart z ∈ coldCylinderSet a A R)
:
(∫ z, (transportDerivative χ (EuclideanFlight.hotChart.symm z)-
χ (EuclideanFlight.hotChart.symm z)*GeometricBackground.frequency
E.phase η E.fraction K α γ z.1.1 z.1.2 z.2)*E.hotLimit z
∂(coldCylinderVolume a A R).prod volume)+
2*(∫ z, χ (EuclideanFlight.hotChart.symm z) ∂incomingGainMeasure
(E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) = 0 := by
have hA : ENNReal.ofReal A < E.horizon :=
(ENNReal.ofReal_le_ofReal hAB.le).trans_lt hB
have hb := E.transport_measure_balance hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα
hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hAB hB hR hχ hc hs hsC
let ψ : HotKineticPhase → ℝ := fun z => χ (EuclideanFlight.hotChart.symm z)
have hψ : Measurable ψ := hχ.continuous.measurable.comp EuclideanFlight.hotChart.symm.measurable
obtain ⟨Cψ,hψB⟩ := hχ.continuous.bounded_above_of_compact_support hc
have hψBound (z) : |ψ z| ≤ Cψ := hψB _
rw [E.toHotLimitExtraction.actual_loss_cylinder_integral ha haA hK hα hγ hq₂ hψ hψBound] at hb
obtain ⟨CD,hDB⟩ := (transportDerivative_continuous hχ).bounded_above_of_compact_support
(transportDerivative_hasCompactSupport hc)
have hd := ((E.toHotLimitExtraction.physical_weak_cylinder S hs₀ ha.le hA R).2.1).bdd_mul
((transportDerivative_continuous hχ).measurable.comp
EuclideanFlight.hotChart.symm.measurable).aestronglyMeasurable
(ae_of_all _ (fun z => hDB (EuclideanFlight.hotChart.symm z)))
dsimp only [Function.comp_def] at hd
have hl := (E.toHotLimitExtraction.actual_loss_cylinder_integrable
(R := R) ha haA hK hα hγ hq₂).bdd_mul hψ.aestronglyMeasurable (ae_of_all _ hψBound)
have he : (∫ z, (transportDerivative χ (EuclideanFlight.hotChart.symm z)-
ψ z*GeometricBackground.frequency E.phase η E.fraction K α γ z.1.1 z.1.2 z.2)*
E.hotLimit z ∂(coldCylinderVolume a A R).prod volume) =
(∫ z, transportDerivative χ (EuclideanFlight.hotChart.symm z)*E.hotLimit z
∂(coldCylinderVolume a A R).prod volume)-
(∫ z, ψ z*(E.hotLimit z*GeometricBackground.frequency E.phase η E.fraction K α γ
z.1.1 z.1.2 z.2) ∂(coldCylinderVolume a A R).prod volume) := by
rw [← integral_sub hd hl]
apply integral_congr_ae
exact ae_of_all _ (fun z => by ring)
change (∫ z, (transportDerivative χ (EuclideanFlight.hotChart.symm z)-
ψ z*GeometricBackground.frequency E.phase η E.fraction K α γ z.1.1 z.1.2 z.2)*
E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+_ = 0
rw [he]
linarith
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # The actual hot transport equation with finite incoming gain and loss measures -/
noncomputable section
open MeasureTheory Filter Set
open scoped ENNReal
open BoltzmannNonuniqueness.TransportCutoff BoltzmannNonuniqueness.CollisionCompactness
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotPairExtraction.separated_transport_measure_balance
(hDP : Published.DunfordPettis1940HotPairWindows)
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2)
{a A B R Rₑ : ℝ} (ha : 0 < a) (haA : a ≤ A) (hAB : A < B)
(hB : ENNReal.ofReal B < E.horizon) (hR : 0 ≤ R)
{χ : Published.KineticPhase → ℝ} (hχ : ContDiff ℝ (⊤ : ℕ∞) χ)
(hc : HasCompactSupport χ) (hs : tsupport χ ⊆ kineticWindow a A Rₑ)
(hsC : ∀ z ∈ tsupport χ, EuclideanFlight.hotChart z ∈ coldCylinderSet a A R)
{θ : ℝ × JetPrototype.Space → ℝ} (hθ : Measurable θ)
{Cθ : ℝ} (hθB : ∀ x, |θ x| ≤ Cθ)
{φ : Velocity → ℝ} (hφ : Continuous φ) {Cφ : ℝ} (hφB : ∀ v, |φ v| ≤ Cφ)
(hsep : ∀ z, χ (EuclideanFlight.hotChart.symm z) = θ z.1*φ z.2) :
(∫ z, transportDerivative χ (EuclideanFlight.hotChart.symm z)*E.hotLimit z
∂(coldCylinderVolume a A R).prod volume)+
2*(∫ z, χ (EuclideanFlight.hotChart.symm z)
∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ
(coldCylinderVolume a A R)))-
(∫ z, χ (EuclideanFlight.hotChart.symm z)
∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ
(coldCylinderVolume a A R))) = 0 := by
let μ := E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)
let _ : SFinite μ := by dsimp [μ,HotLimitExtraction.mixedMeasure]; infer_instance
have hi : Integrable incomingRate μ :=
E.toHotLimitExtraction.incomingRate_integrable ha (ha.le.trans haA) hK hα hγ hq₂
have hCθ : 0 ≤ Cθ := (abs_nonneg (θ (0,0))).trans (hθB _)
have hg := incomingGainMeasure_separated hi hθ hCθ hθB hφ.measurable hφB
have hl := incomingLossMeasure_separated hi hθ hCθ hθB hφ.measurable hφB
simp_rw [hsep]
change _+2*(∫ z, θ z.1*φ z.2 ∂incomingGainMeasure μ)-
(∫ z, θ z.1*φ z.2 ∂incomingLossMeasure μ) = 0
rw [hg,hl]
have hb := E.separated_transport_balance hDP hcarleman hGLPS hs₀ hsmax hη hηmax
hK hα hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hAB hB hR hχ hc hs hsC
hθ hθB hφ hφB hsep
dsimp only [μ] at hg hl ⊢
linarith
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # The actual hot-limit equation tested in characteristic coordinates -/
noncomputable section
open MeasureTheory Set
open scoped ENNReal
open BoltzmannNonuniqueness.TransportCutoff BoltzmannNonuniqueness.CollisionCompactness
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotPairExtraction.characteristic_test_balance
(hDP : Published.DunfordPettis1940HotPairWindows)
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2)
{a A B R Rₑ : ℝ} (ha : 0 < a) (haA : a ≤ A) (hAB : A < B)
(hB : ENNReal.ofReal B < E.horizon) (hR : 0 ≤ R)
{ψ : EuclideanFlight.CharacteristicPhase → ℝ}
(hψ : ContDiff ℝ (⊤ : ℕ∞) ψ) (hc : HasCompactSupport ψ)
(hs : tsupport (EuclideanFlight.testPullback ψ) ⊆ kineticWindow a A Rₑ)
(hsC : ∀ z ∈ tsupport (EuclideanFlight.testPullback ψ),
EuclideanFlight.hotChart z ∈ coldCylinderSet a A R) :
(∫ z, EuclideanFlight.timeDerivative ψ
(EuclideanFlight.characteristicEquiv.symm (EuclideanFlight.hotChart.symm z))*E.hotLimit z
∂(coldCylinderVolume a A R).prod volume)+
(2*(∫ z, ψ (EuclideanFlight.characteristicEquiv.symm (EuclideanFlight.hotChart.symm z))
∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ
(coldCylinderVolume a A R)))-
(∫ z, ψ (EuclideanFlight.characteristicEquiv.symm (EuclideanFlight.hotChart.symm z))
∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ
(coldCylinderVolume a A R)))) = 0 := by
have hb := E.transport_measure_balance hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα
hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA hAB hB hR
(EuclideanFlight.testPullback_contDiff hψ) (EuclideanFlight.testPullback_compact hc) hs hsC
simp_rw [EuclideanFlight.transportDerivative_testPullback hψ] at hb
exact hb
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # Cumulative collision balance for the actual weak hot limit
Every smooth nonnegative compact phase test has an almost-everywhere time trace
given by a constant and the cumulative incoming gain minus incoming loss.
Both source measures are built from the actual mixed atomic-cold/hot measure.
-/
noncomputable section
open MeasureTheory Set
open scoped NNReal ENNReal
open BoltzmannNonuniqueness.CollisionCompactness BoltzmannNonuniqueness.EuclideanFlight
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
def HotLimitExtraction.characteristicGainMeasure (E : HotLimitExtraction S)
{a : ℝ} (ha : 0 < a) (hK : 0 ≤ K) (hα : 0 < α) (hγ : 0 < γ) (A R : ℝ) :
Measure CharacteristicPhase :=
(2 : ℝ≥0) • sourcePullback
(incomingGainMeasure (E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))
def HotLimitExtraction.characteristicLossMeasure (E : HotLimitExtraction S)
{a : ℝ} (ha : 0 < a) (hK : 0 ≤ K) (hα : 0 < α) (hγ : 0 < γ) (A R : ℝ) :
Measure CharacteristicPhase :=
sourcePullback
(incomingLossMeasure (E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))
theorem HotPairExtraction.characteristic_cumulative_balance
(hDP : Published.DunfordPettis1940HotPairWindows)
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2)
{a A B : ℝ} (ha : 0 < a) (haA : a < A) (hAB : A < B)
(hB : ENNReal.ofReal B < E.horizon)
{φ : Velocity × Velocity → ℝ} (hφ : ContDiff ℝ (⊤ : ℕ∞) φ)
(hc : HasCompactSupport φ) (hn : ∀ p, 0 ≤ φ p) :
∃ R : ℝ, 0 ≤ R ∧ ∃ c : ℝ, ∀ᵐ t ∂volume, t ∈ Ioo a A →
WeakTime.phaseProjection (cylinderPullback a A R E.hotLimit) φ t =
c+WeakTime.cumulative (WeakTime.timeSource
(E.toHotLimitExtraction.characteristicGainMeasure ha hK hα hγ A R) φ) t-
WeakTime.cumulative (WeakTime.timeSource
(E.toHotLimitExtraction.characteristicLossMeasure ha hK hα hγ A R) φ) t := by
obtain ⟨R,Rₑ,hR,hloc⟩ := exists_timePhase_cylinder a A hc
refine ⟨R,hR,?_⟩
let μ := E.toHotLimitExtraction.characteristicGainMeasure ha hK hα hγ A R
let ν := E.toHotLimitExtraction.characteristicLossMeasure ha hK hα hγ A R
let _ := E.toHotLimitExtraction.incomingGainMeasure_finite
(R := R) ha (ha.le.trans haA.le) hK hα hγ hq₂
let _ := E.toHotLimitExtraction.incomingLossMeasure_finite
(R := R) ha (ha.le.trans haA.le) hK hα hγ hq₂
have : IsFiniteMeasure μ := by dsimp [μ,HotLimitExtraction.characteristicGainMeasure]; infer_instance
have : IsFiniteMeasure ν := by dsimp [ν,HotLimitExtraction.characteristicLossMeasure]; infer_instance
obtain ⟨C,hC⟩ := hφ.continuous.bounded_above_of_compact_support hc
have hi := (E.toHotLimitExtraction.physical_weak_cylinder S hs₀ ha.le
((ENNReal.ofReal_le_ofReal hAB.le).trans_lt hB) R).2.1
apply WeakTime.projected_cumulative_balance haA (cylinderPullback_integrable hi)
hφ.continuous.measurable hn hC μ ν
intro θ hθ hθc hθs
have hlocθ := hloc θ hθs
have hb := E.characteristic_test_balance hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα
hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA.le hAB hB hR
(timePhaseTest_contDiff hθ hφ) (timePhaseTest_compact hθc hc) hlocθ.1 hlocθ.2
simp_rw [timeDerivative_timePhaseTest hθ hφ] at hb
rw [cylinderPullback_integral]
have hm : Measurable (fun z : CharacteristicPhase => θ z.1*φ z.2) :=
(hθ.continuous.measurable.comp measurable_fst).mul
(hφ.continuous.measurable.comp measurable_snd)
change _ + (∫ z, θ z.1*φ z.2 ∂((2 : ℝ≥0) • sourcePullback _))-
(∫ z, θ z.1*φ z.2 ∂sourcePullback _) = 0
rw [integral_smul_nnreal_measure,sourcePullback_integral _ hm,sourcePullback_integral _ hm]
change _ + 2*(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2
∂incomingGainMeasure (E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) - _ = 0
change (∫ z, (deriv θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2)*
E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+
(2*(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2
∂incomingGainMeasure (E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))-
(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2
∂incomingLossMeasure (E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) = 0 at hb
linarith only [hb]
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # The actual weak-balance cylinder also covers the full compact phase support -/
noncomputable section
open MeasureTheory Set
open scoped NNReal ENNReal
open BoltzmannNonuniqueness.CollisionCompactness BoltzmannNonuniqueness.EuclideanFlight
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotPairExtraction.covered_characteristic_weak_balance
(hDP : Published.DunfordPettis1940HotPairWindows)
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2)
{a A B : ℝ} (ha : 0 < a) (haA : a < A) (hAB : A < B)
(hB : ENNReal.ofReal B < E.horizon)
{β : Velocity × Velocity → ℝ} (hβc : HasCompactSupport β) :
∃ R : ℝ, 0 ≤ R ∧
(∀ t ∈ Icc a A, ∀ p ∈ tsupport β, hotCharacteristicEquiv (t,p) ∈ coldCylinderSet a A R) ∧
∀ φ : WeakTime.Phase → ℝ,
ContDiff ℝ (⊤ : ℕ∞) φ → HasCompactSupport φ → (∀ p, 0 ≤ φ p) →
tsupport φ ⊆ tsupport β → ∀ θ : ℝ → ℝ,
ContDiff ℝ (⊤ : ℕ∞) θ → HasCompactSupport θ → tsupport θ ⊆ Ioo a A →
(∫ z, (deriv θ z.1*φ z.2)*cylinderPullback a A R E.hotLimit z)+
(∫ z, θ z.1*φ z.2 ∂E.toHotLimitExtraction.characteristicGainMeasure ha hK hα hγ A R)-
(∫ z, θ z.1*φ z.2 ∂E.toHotLimitExtraction.characteristicLossMeasure ha hK hα hγ A R) = 0 := by
obtain ⟨R₀,Rₑ,hR₀,hloc⟩ := exists_timePhase_cylinder_for_support a A hβc
obtain ⟨R₁,_hR₁,hcover⟩ := exists_phase_cylinder a A hβc
let R := max R₀ R₁
have hR : 0 ≤ R := hR₀.trans (le_max_left _ _)
refine ⟨R,hR,?_,?_⟩
· intro t ht p hp
exact coldCylinderSet_mono_radius (le_max_right _ _) (hcover t ht p hp)
intro φ hφ hc _hn hφβ θ hθ hθc hθs
have hlocθ := hloc φ hφβ θ hθs
have hcoverθ : ∀ z ∈ tsupport (testPullback (timePhaseTest θ φ)),
hotChart z ∈ coldCylinderSet a A R := fun z hz =>
coldCylinderSet_mono_radius (le_max_left _ _) (hlocθ.2 z hz)
have hb := E.characteristic_test_balance hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα
hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA.le hAB hB hR
(timePhaseTest_contDiff hθ hφ) (timePhaseTest_compact hθc hc) hlocθ.1 hcoverθ
simp_rw [timeDerivative_timePhaseTest hθ hφ] at hb
rw [cylinderPullback_integral]
have hm : Measurable (fun z : CharacteristicPhase => θ z.1*φ z.2) :=
(hθ.continuous.measurable.comp measurable_fst).mul
(hφ.continuous.measurable.comp measurable_snd)
change _ + (∫ z, θ z.1*φ z.2 ∂((2 : ℝ≥0) • sourcePullback _))-
(∫ z, θ z.1*φ z.2 ∂sourcePullback _) = 0
rw [integral_smul_nnreal_measure,sourcePullback_integral _ hm,sourcePullback_integral _ hm]
change (∫ z, (deriv θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2)*
E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+
(2*(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2
∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))))-
(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2
∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) = 0
change (∫ z, (deriv θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2)*
E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+
((2*(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2
∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))))-
(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2
∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) = 0 at hb
linarith only [hb]
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # The actual characteristic gain is the sum of both outgoing collision laws
This identity uses the physical normal-collision law for the mixed measure,
including its atomic cold partner. No density Carleman identity is used here.
-/
noncomputable section
open MeasureTheory
open scoped NNReal ENNReal
open BoltzmannNonuniqueness.CollisionCompactness BoltzmannNonuniqueness.EuclideanFlight
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotLimitExtraction.characteristicGain_test_integral (E : HotLimitExtraction S)
{a A R : ℝ} (ha : 0 < a) (haA : a ≤ A) (hK : 0 ≤ K) (hα : 0 < α) (hγ : 0 < γ)
(hq : q < 2) {ψ : CharacteristicPhase → ℝ} (hψ : Measurable ψ)
{B : ℝ} (hB : ∀ u, |ψ u| ≤ B) :
(∫ u, ψ u ∂E.characteristicGainMeasure ha hK hα hγ A R) =
∫ z, ψ (hotCharacteristicEquiv.symm (incomingLeft z))+
ψ (hotCharacteristicEquiv.symm (incomingRight z))
∂incomingCollisionMeasure (E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)) := by
let μ := E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)
let _ : SFinite μ := by dsimp [μ,HotLimitExtraction.mixedMeasure]; infer_instance
have hi : Integrable incomingRate μ := E.incomingRate_integrable ha (ha.le.trans haA) hK hα hγ hq
let _ := incomingCollisionMeasure_finite hi
have hm : Measurable (fun z : HotKineticPhase => ψ (hotCharacteristicEquiv.symm z)) :=
hψ.comp hotCharacteristicEquiv.symm.measurable
have hL : Integrable (fun z => ψ (hotCharacteristicEquiv.symm (incomingLeft z)))
(incomingCollisionMeasure μ) :=
(integrable_const B).mono' (hm.comp incomingLeft_measurable).aestronglyMeasurable
(ae_of_all _ (fun z => hB _))
have hR : Integrable (fun z => ψ (hotCharacteristicEquiv.symm (incomingRight z)))
(incomingCollisionMeasure μ) :=
(integrable_const B).mono' (hm.comp incomingRight_measurable).aestronglyMeasurable
(ae_of_all _ (fun z => hB _))
rw [HotLimitExtraction.characteristicGainMeasure,integral_smul_nnreal_measure,
sourcePullback_integral _ hψ,incomingGainMeasure_integral hi hm (fun z => hB _)]
change 2*((1/2 : ℝ)*_)=_
rw [integral_add hL hR]
ring
theorem HotLimitExtraction.characteristicGain_normal_integral (E : HotLimitExtraction S)
{a A R : ℝ} (ha : 0 < a) (haA : a ≤ A) (hK : 0 ≤ K) (hα : 0 < α) (hγ : 0 < γ)
(hq : q < 2) {ψ : CharacteristicPhase → ℝ} (hψ : Measurable ψ)
{B : ℝ} (hB : ∀ u, |ψ u| ≤ B) :
(∫ u, ψ u ∂E.characteristicGainMeasure ha hK hα hγ A R) =
∫ p, ∫ ω, collisionKernel p.2.1 p.2.2 ω*
(ψ (hotCharacteristicEquiv.symm (incomingLeft (p,ω)))+
ψ (hotCharacteristicEquiv.symm (incomingRight (p,ω)))) ∂sphereArea
∂E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R) := by
let μ := E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)
let _ : SFinite μ := by dsimp [μ,HotLimitExtraction.mixedMeasure]; infer_instance
rw [E.characteristicGain_test_integral ha haA hK hα hγ hq hψ hB]
apply incomingCollisionMeasure_integral_prod
(E.incomingRate_integrable ha (ha.le.trans haA) hK hα hγ hq)
· exact ((hψ.comp hotCharacteristicEquiv.symm.measurable).comp incomingLeft_measurable).add
((hψ.comp hotCharacteristicEquiv.symm.measurable).comp incomingRight_measurable)
· intro z
exact (abs_add_le _ _).trans ((add_le_add (hB _) (hB _)).trans_eq (two_mul B).symm)
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # One physical cylinder for the actual weak balance of all local phase tests -/
noncomputable section
open MeasureTheory Set
open scoped NNReal ENNReal
open BoltzmannNonuniqueness.CollisionCompactness BoltzmannNonuniqueness.EuclideanFlight
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotPairExtraction.common_characteristic_weak_balance
(hDP : Published.DunfordPettis1940HotPairWindows)
(hcarleman : Published.GPV2009CarlemanInput) (hGLPS : Published.GLPS1988Proposition3)
(E : HotPairExtraction S)
(hs₀ : 0 < s₀) (hsmax : s₀ ≤ 1/8) (hη : 0 < η) (hηmax : η ≤ Real.log 2)
(hK : 0 ≤ K) (hα : 0 < α) (hαmax : α ≤ 1/4) (hγ : 0 < γ)
(hd₀ : 0 < d₀) (hd₀max : d₀ ≤ 1)
(hsmall : JetComparisonCoefficient.coefficient K*d₀*s₀^9 ≤ 1)
(hq₁ : 1 < q) (hq₂ : q < 2)
{a A B : ℝ} (ha : 0 < a) (haA : a < A) (hAB : A < B)
(hB : ENNReal.ofReal B < E.horizon)
{β : Velocity × Velocity → ℝ} (hβc : HasCompactSupport β) :
∃ R : ℝ, 0 ≤ R ∧ ∀ φ : WeakTime.Phase → ℝ,
ContDiff ℝ (⊤ : ℕ∞) φ → HasCompactSupport φ → (∀ p, 0 ≤ φ p) →
tsupport φ ⊆ tsupport β → ∀ θ : ℝ → ℝ,
ContDiff ℝ (⊤ : ℕ∞) θ → HasCompactSupport θ → tsupport θ ⊆ Ioo a A →
(∫ z, (deriv θ z.1*φ z.2)*cylinderPullback a A R E.hotLimit z)+
(∫ z, θ z.1*φ z.2 ∂E.toHotLimitExtraction.characteristicGainMeasure ha hK hα hγ A R)-
(∫ z, θ z.1*φ z.2 ∂E.toHotLimitExtraction.characteristicLossMeasure ha hK hα hγ A R) = 0 := by
obtain ⟨R,Rₑ,hR,hloc⟩ := exists_timePhase_cylinder_for_support a A hβc
refine ⟨R,hR,?_⟩
intro φ hφ hc _hn hφβ θ hθ hθc hθs
have hlocθ := hloc φ hφβ θ hθs
have hb := E.characteristic_test_balance hDP hcarleman hGLPS hs₀ hsmax hη hηmax hK hα
hαmax hγ hd₀ hd₀max hsmall hq₁ hq₂ ha haA.le hAB hB hR
(timePhaseTest_contDiff hθ hφ) (timePhaseTest_compact hθc hc) hlocθ.1 hlocθ.2
simp_rw [timeDerivative_timePhaseTest hθ hφ] at hb
rw [cylinderPullback_integral]
have hm : Measurable (fun z : CharacteristicPhase => θ z.1*φ z.2) :=
(hθ.continuous.measurable.comp measurable_fst).mul
(hφ.continuous.measurable.comp measurable_snd)
change _ + (∫ z, θ z.1*φ z.2 ∂((2 : ℝ≥0) • sourcePullback _))-
(∫ z, θ z.1*φ z.2 ∂sourcePullback _) = 0
rw [integral_smul_nnreal_measure,sourcePullback_integral _ hm,sourcePullback_integral _ hm]
change (∫ z, (deriv θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2)*
E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+
(2*(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2
∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))))-
(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2
∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))) = 0
change (∫ z, (deriv θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2)*
E.hotLimit z ∂(coldCylinderVolume a A R).prod volume)+
((2*(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2
∂incomingGainMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R))))-
(∫ z, θ (hotCharacteristicEquiv.symm z).1*φ (hotCharacteristicEquiv.symm z).2
∂incomingLossMeasure (E.toHotLimitExtraction.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)))) = 0 at hb
linarith only [hb]
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
section
/-! # The actual characteristic gain as a hot-particle and cold-partner integral -/
noncomputable section
open MeasureTheory ProbabilityTheory
open scoped ProbabilityTheory
open BoltzmannNonuniqueness.CollisionCompactness BoltzmannNonuniqueness.EuclideanFlight
namespace BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
variable {s₀ η K α γ d₀ q : ℝ} {F : ShrinkingCapFamily s₀ η K α γ d₀ q}
{S : AttainedCapSequence F}
theorem HotLimitExtraction.characteristicGain_hot_integral (E : HotLimitExtraction S)
{a A R : ℝ} (ha : 0 < a) (haA : a ≤ A) (hK : 0 ≤ K) (hα : 0 < α) (hγ : 0 < γ)
(hq : q < 2) {ψ : CharacteristicPhase → ℝ} (hψ : Measurable ψ)
{B : ℝ} (hB : ∀ u, |ψ u| ≤ B) :
(∫ u, ψ u ∂E.characteristicGainMeasure ha hK hα hγ A R) =
∫ x, ∫ w, E.cappedHot (x,w)*
(∫ v, ∫ ω, collisionKernel v w ω*
(ψ (hotCharacteristicEquiv.symm (x,scatterLeft v w ω))+
ψ (hotCharacteristicEquiv.symm (x,scatterRight v w ω))) ∂sphereArea
∂E.background (max a x.1) x.2) ∂volume ∂coldCylinderVolume a A R := by
let μ := E.mixedMeasure ha hK hα hγ (coldCylinderVolume a A R)
let _ : SFinite μ := by dsimp [μ,HotLimitExtraction.mixedMeasure]; infer_instance
let f : ((ℝ × JetPrototype.Space) × (Velocity × Velocity)) × Sphere → ℝ := fun z =>
ψ (hotCharacteristicEquiv.symm (incomingLeft z))+
ψ (hotCharacteristicEquiv.symm (incomingRight z))
have hm : Measurable f :=
((hψ.comp hotCharacteristicEquiv.symm.measurable).comp incomingLeft_measurable).add
((hψ.comp hotCharacteristicEquiv.symm.measurable).comp incomingRight_measurable)
have hb (z) : |f z| ≤ 2*B :=
(abs_add_le _ _).trans ((add_le_add (hB _) (hB _)).trans_eq (two_mul B).symm)
have hi := incomingCollision_weight_integrable
(E.incomingRate_integrable (R := R) ha (ha.le.trans haA) hK hα hγ hq) hm hb
have hF : Integrable (fun p => ∫ ω, collisionKernel p.2.1 p.2.2 ω*f (p,ω) ∂sphereArea) μ :=
hi.integral_prod_left
rw [E.characteristicGain_normal_integral ha haA hK hα hγ hq hψ hB]
change (∫ p, (∫ ω, collisionKernel p.2.1 p.2.2 ω*f (p,ω) ∂sphereArea)
∂(coldCylinderVolume a A R ⊗ₘ E.mixedKernel ha hK hα hγ)) = _
rw [Measure.integral_compProd hF]
apply integral_congr_ae
filter_upwards [(Measure.integrable_compProd_iff hF.aestronglyMeasurable).mp hF |>.1] with x hx
let _ : IsFiniteMeasure (E.background (max a x.1) x.2) :=
GeometricBackground.background_finite E.phase η E.fraction K α γ (max a x.1) x.2
rw [E.mixedKernel_apply] at hx ⊢
rw [integral_prod_symm _ hx,E.hotKernel_integral]
rfl
end BoltzmannNonuniqueness.JetCopyDatum.AttainedCapSequence
end
end
end OAI