Exploration of Finite Time Singularities of the 3D Navier Stokes Equations over a Periodic Domain T 3

Terry Moschandreou
Terry Moschandreou * § Doctor of Philosophy Applied Mathematics
§ Intermediate Science and Mathematics

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Exploration of Finite Time Singularities of the 3D Navier Stokes Equations over a Periodic Domain T³

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Abstract

This paper develops a structured analytical framework for the three-dimensional incompressible Navier-Stokes equations based on recursive compositions of the Lambert W function and successive algebraic transformations of the nonlinear inertial terms. A hierarchy of derived vector fields is constructed using systematic row-operation transformations involving multiplication by scalar fields, addition of equations, and repeated application of the product rule. These transformations generate a closed sequence of transport equations that preserve the algebraic structure of the original Navier–Stokes system. Work by the corresponding author has been carried out recently where a non-smooth periodic attractor has been shown to exist for the Navier–Stokes problem on T 3 , and an acceleration ratio measuring the relative scaling of temporal and mixed derivatives in a specific composition hierarchy is shown to exist. It is presently shown that the solution of the Navier–Stokes equations in terms of the Weierstrass Zeta function with this ratio, which is dependent on the Lambert W function, leads to a higher derivative (order 2 ) blowup in finite time. It is of interest that one component must blow up pointwise in finite time out of the three when seeking C solutions for the other two. If a singularity occurs, at least one component must blow up pointwise. Two components cannot remain smooth while the system develops a singularity without the third blowing up. If a finite-time singularity occurs, then u z . A central result of the analysis is the derivation of compact recursive formulas for spatial and temporal derivatives of iterated Lambert W compositions, expressed as finite products of factors of the form ( 1 + W j ) . Repeated integration by parts yields a finite algebraic representation in which all integral terms collapse into boundary contributions, establishing an explicit closed-form structure for the resulting expressions. Within the transformed hierarchy, an exact identity is established between nonlinear gradient production and viscous diffusion terms. This equality implies that the combined field reduces to a pure divergence structure on periodic domains, yielding a precise mathematical interpretation of the statement “production equals diffusion.” Explicit solutions of the resulting scalar transport equations are obtained in closed form using the Lambert W function. The analysis shows that the critical branch condition of the Lambert function produces a finite-value solution while its spatial gradient becomes unbounded, representing a loss of smoothness rather than divergence of the solution amplitude at t1

  1. Introduction
  2. The generalized ratio R n
  3. Calculation of I n   d z
  4. Integral of the Nested Product Expression
    1. 1. Fundamental Dimensions
    2. 2. Definition of Refinement Geometry
    3. 3. Dimensional analysis
    4. 4. Geometric Interpretation
    5. 5. Time Dependence and Interpretation
    6. 6. Refinement Rate (Optional Dynamic Quantity)
    7. 7. Final Summary
  5. Proof that I n 0 as n
    1. Lambert w function and Branch Point Structure
    2. Iteration of Analytic Functions
    3. Recursive Derivative Chains
    4. Asymptotic Estimates and Limit evaluation
    5. Structural Interpretation
    6. Behavior of W j near the branch point
    7. Behavior of the derivatives W j
  6. Decay of the derivatives in iterated Lambert W
    1. Derivative recursion
    2. Asymptotic expansion near zero
    3. Asymptotic behavior of W j
    4. Product estimate
    5. Conclusion
    6. Asymptotic behavior of the mixed product expression
    7. Step 1: Fundamental asymptotics of the iterated Lambert W sequence
    8. Step 2: Product of derivatives up to k ( n )
    9. Step 3: Remaining product of ( 1 + W i )
    10. Step 4: Assemble the full asymptotic
    11. Step 5: Key regimes
      1. Case 1: k ( n ) = n
      2. Case 2: k ( n ) = α n with 0 < α < 1
      3. Case 3: k ( n ) = log n
    12. Final conclusion
    13. Structural reason
    14. Convergence of the series n = 1 A n
    15. Conclusion
  7. Row Operations Reducing ( u ) u to b b
  8. 1. Convective terms of the three momentum equations
  9. 2. Row operations
    1. Operation A (produces the k -component)
    2. Operation B (produces the i -component)
    3. Operation C (produces the j -component)
  10. 3. Matrix representation of the row operations
  11. 4. Product rule
  12. 5. Definition of the vector field b
  13. 6. Second application of the same row operations
  14. 7. Complete hierarchy
  15. Construction of ( b ) a from ( b ) b
    1. Definitions
    2. The inertial operator acting on b
    3. Multiply by u z
    4. Multiply the z -momentum equation by b
    5. Add the two expressions
    6. Apply the product rule
    7. Recognize the transported vector field
    8. Fully expanded component form
  16. Final Transformation identity
  17. Structural interpretation
  18. Extension of the Row-Operation Construction to All Navier–Stokes Terms
    1. 1. The full 3D Navier–Stokes equations
    2. 2. Transformation operator
    3. 3. Definition of the derived vector field
    4. 4. Time derivative transformation
    5. Inertial term transformation
  19. Successive Matrix Operations on the Viscous Term
    1. 1. Navier–Stokes viscous term
    2. 2. Definition of the first derived vector field
    3. 3. First row-operation matrix
    4. 4. Second derived vector field
    5. 5. Second row-operation matrix
    6. 6. Laplacian product rule for vector fields
    7. 7. Successive matrix transformation
    8. Final structural identity
  20. Successive Matrix Transformations of the Pressure Gradient Term
    1. 1. Pressure gradient term in the Navier–Stokes equations
    2. 2. Definition of the velocity vector
    3. 3. Definition of the first derived vector field
    4. 4. Definition of the second derived vector field
    5. 5. First row-operation matrix
    6. First component
    7. 6. Second row-operation matrix
    8. 7. Product rule for gradient of scalar-vector product
    9. 8. Successive matrix transformation
    10. Final structural identity
  21. Successive Matrix Transformations of the Force Field and Final Navier–Stokes Form
    1. 1. Original Navier–Stokes equations
    2. 2. Derived vector fields
    3. 3. Matrix operators
  22. 4. Force Field Transformation
    1. Original force term
    2. 5. First transformation
    3. 6. Second transformation
  23. Summary of all transformed terms
    1. Time derivative
    2. Inertial term
    3. Pressure term
    4. Viscous term
    5. Force term
  24. Final transformed Navier–Stokes equation
  25. Final hierarchical Navier–Stokes structure
  26. Meaning of Production = Diffusion
    1. 1) Starting identity
    2. 2) Definition of production
    3. 3) Definition of diffusion
    4. 4) Exact meaning of Production = Diffusion
    5. 5) Structural consequence
    6. 6) Consequence on the periodic torus
    7. 7) Physical interpretation
    8. 8) Analogy with classical Navier–Stokes energy balance
    9. Final precise definition
  27. The existence of a LambertW solution of the governing equations of Fluid Mechanics
    1. A unique representation for the PNS system
  28. Difference between
    u z = LambertW ( exp ( G ( x , y , z , t ) 1 ) )
    and constant k ( n ) multipliers
  29. No Finite-Time Blowup of b and Blowup of Higher Time Derivatives
  30. Solution of u z PDE and definition of f 1 , f 2 and f 3
  31. Logic structure of singularities of NS Analysis of equation
  32. 1) First logical consequence from u x u y blowup
  33. 2) Use the second product
  34. 3) Combine both statements
  35. Analysis of 1 / ( sin ( Z t ) + 1 ϵ ) and 1 / ( sin ( Z t ) + 1 )
    1. Denominator bounds
    2. Check for zeros
    3. Finite-time blowup
    4. Comparison with ϵ > 2
    5. Conclusion
  36. Analysis of the Function f ( Z , t ) = 1 η + sin ( Z t ) + 1 ϵ
    1. Blowup condition
    2. Use the boundedness of sine
    3. Solve the inequality
  37. Final classification of finite time blowup
    1. Finite-time blowup occurs if and only if
    2. No finite-time blowup occurs if and only if
  38. Useful special cases
    1. Case 1 Original blowup case
    2. Case 2 Small positive regularization
    3. Case 3 Large negative shift
  39. Interpretation
  40. General Transport Structure of b 3 , u y inputs:How PDE re-enters a square term
  41. General Finite time blowup after gradient blowup
  42. Transport Structure and Regularity Properties of the b 3 Solution
  43. Listing of Matlab Code for the PDE with b 2 term
    1. Characteristic transport formulation
    2. Explicit Lambert W representation
    3. Branch singularity structure
    4. First-order regularity
    5. Behavior at z = t + π / 2
    6. Behavior at z = t π / 2
    7. Failure of second-order regularity
    8. Final conclusion
  44. Defining F ( x , y , ξ ( z ) ) uniquely to obtain the branch point of the LambertW function at z = z = t + π 2
    1. Finalized expression for b 3
  45. Mathematical Description
  46. Mathematical Context
  47. Foliations
  48. Step 1 — Compute the Gradient
  49. Step 2 — Determine the level Sets
  50. Step 3 — Show the Sets Partition the Space
  51. Step 4 — Verify the Local Coordinate condition (Definition of Foliation)
  52. Geometric Meaning
  53. Conclusion
  54. Useful General Principle
  55. Proof that b 1 u z x + b 2 u z y = 0 through foliations y = x + C where C R
    1. Substitute the foliation
    2. Impose the condition f 2 = f 1
    3. Add u x + u y
    4. Conclusion
  56. Geometric compatibility analysis for f 1 = α f 2 3
  57. Compatibility PDE when f 1 = α f 2 3 and α = α ( x , y )
  58. 1. Express f 2 in terms of f 1 , α
  59. 2. New geometric decomposition
  60. 3. Because α = α ( x , y )
  61. 4. Explicit consequence for blow-up
    1. The Irrotational “Shock” Realization
  62. Proof that u z y + u y z = u z x + u x z along a plane foliation
  63. Collection of terms with Pressure P and u z defining ( f a ) z (force in z direction)
  64. Proof of Periodicity of u x provided ϵ 3 0
  65. Explicit Formula for u x
  66. Periodicity in z
  67. Periodicity of the Lambert W Composition
  68. Membership in the One-Dimensional Torus
  69. Analysis of the Modified Denominator
  70. Critical Geometry
  71. Behavior of the Lambert Argument
  72. Regularity Consequences
  73. 7. Final Statement
  74. Analysis of ϵ 3 u x u y for the Modified Structure 1 sin ( t z + ϵ ) + ϵ 3
  75. 1. Definitions
  76. 2. Identification of the Singular Point
  77. 3. Gradient of u y
  78. 4. Behavior of the Lambert- W Derivative
  79. 5. Gradient of u x
  80. 6. Dot Product Scaling
  81. 7. Multiply by ϵ 3
  82. 8. Integral behavior
  83. Geometric difference from the Previous case
  84. Final Conclusion
  85. Condition for Vanishing
  86. Viscosity Scaling and Vanishing of the Gradient Product Term
  87. 1. Asymptotic scaling of the gradient product
  88. 2. Integral on the torus
  89. 3. Localized collapse under vanishing support
  90. 4. Conclusion
  91. A smooth extension of the Navier Stokes equations
  92. Regularized Transport Equation for the Transformed Variable
    1. Interpretation
    2. Energy Identity
  93. Hyperviscous Extension of the Transformed Navier–Stokes system
  94. The Governing PDE for the i th flow direction
  95. Coefficient PDE of the e 2 V 3 Term
  96. Full PDE Combining the e 2 v 3 and e v 3 Contributions
  97. Verification and Reduction of the Nonlinear PDE
  98. Ansatz
  99. Factorization Identity
  100. Derivatives of D
  101. Derivatives of H
  102. First Derivatives of v 3
    1. y 3 -Derivative
    2. y 1 -Derivative
    3. s -Derivative
  103. Mixed Derivative v 3 , y 1 y 3
    1. Derivative of the Singular Part
    2. Derivative of the H -Part
  104. Substitution into the PDE
  105. Exact Cancellation
  106. Reduced Equation
  107. Transport Equation
  108. Characteristic solution
  109. Smooth Initial data Formulation
  110. Final Result
  111. Automatic Smoothness of the Transformed Variable v 3
  112. 1. Compute the Exact Form of V 3
  113. 2. Recovering H from V 3
  114. 3. Smooth Initial data
  115. 4. Recovering F
  116. 5. Recovering Λ
  117. 6. Propagation Along characteristics
  118. 7. Final Conclusion
  119. Nonlinear Coupled Structure with v 3 -Dependent Coefficients
  120. 1. Derivatives of V 3
  121. 2. Coefficients depending on v 3
  122. 3. Leading-order singular structure
  123. 4. Lambert W structure in b 3 and induced behavior
  124. 5. Coupling to v 3
  125. 6. Integral over T 3
  126. 7. Correct interpretation of the singular structure
  127. Final Conclusion
  128. Analysis of the integrand
  129. Structure of the Integrand
  130. Definition of the Integral
  131. Evaluation of the One-Dimensional Integral
  132. Asymptotic Regimes
    1. Case 1: λ < 0
    2. Case 2: L with fixed v 0
  133. Verification of the Key Claim
  134. Conclusion
  135. Analysis of the integral I and consistency of the exponential ansatz
  136. Scaling of the nonlinear integrand
  137. Evaluation of the torus integral
  138. Asymptotic regimes
    1. Case λ < 0
    2. Case λ > 0
  139. Consistency of the scaling with expanding tori
    1. Large-data regime.
  140. Physical interpretation
  141. Conclusion
  142. Lambert W Branch Point Scaling and Large Initial Data Suppression
  143. 1. Lambert W Branch Point Condition
  144. 2. Value of W at the Branch Point
  145. 3. How to Make the Whole Expression Small
  146. 4. Natural Scaling Choice
  147. 5. Minimal Decay Choice
  148. 6. Exact Branchpoint-Compatible Choice
  149. 7. Strongest Stable Choice
  150. 8. Branch Expansion Confirmation
  151. Can v 1 or v 1 = v 1 / δ be non smooth?
  152. 1. At z = t + π 2
    1. First derivative
  153. 2. At z = t π 2
    1. First derivative there
  154. Higher derivatives
  155. Final summary
  156. u z = u z / δ behaviour cancellation
  157. Expression b 3 = b 3 / δ
  158. Behavior near the branch point
  159. Differentiate the full expression
  160. On the n th compositions of LambertW functions and their solution to Equation (33)
  161. Conclusion
  162. Appendix A
  163. The General Ratio R n
  164. LambertW Composition with Terminal ( 1 + W j ) Factors
  165. Derivative of the LambertW function
  166. First-level derivatives
  167. Recursive derivatives
  168. Proof of the Compact Product Formula for z W n and t W n
  169. Base case n = 1
  170. Recursive derivative relation
  171. Induction hypothesis
  172. Inductive step
  173. Conclusion
  174. Final Result
  175. Mixed derivative
  176. Derivation of the Mixed Derivative t z W n
  177. Apply the quotient rule
  178. Substitute known derivative
  179. Differentiate the product P n
  180. Substitute into mixed derivative
  181. Telescoping structure
  182. Final simplification
  183. Final Result
  184. Ratio of derivatives
  185. Integrand for the velocity potential
  186. Conclusion
  187. Appendix B
    1. Step 0: Setup
    2. Integration by parts formula
    3. First integration by parts
    4. Repeat n 1 times
    5. Final closed form after n 1 steps
    6. Examples for small n
  188. Proof of the Derivative Structure Used here
  189. Proof of the Derivative Structure
    1. Goal
    2. Write the function as a Product
    3. Differentiate using the Product Rule
    4. Compute the Derivative of the Product
    5. Differentiate the Square-Root Term
    6. Substitute Both Derivatives
    7. Insert the Factor ( 1 + W n ) 3 / 2
    8. Identify H 0 ( z )
    9. Immediate Consequence
    10. Structural Remark
  190. Proof of and Repeated Integration by Parts
  191. First Integration by Parts
  192. Structure of the New Integrand
  193. Repetition of the Procedure
  194. Inductive Reduction
  195. Termination After ( n 1 ) Steps
  196. Final Result
  197. Origin of the Division by H k ( z ) in the Final Expression
  198. Integration by Parts Step
  199. Key Observation
  200. Recursive Structure
  201. Final Expression
  202. Conclusion
  203. Full Proofs of Steps 2 and 3
  204. Proof of and Step 3
  205. Product Rule Differentiation
    1. Theorem (Product Rule)
    2. Application
  206. Derivative of the Power Term
    1. Chain Rule
  207. Derivative of the Product P ( z )
    1. Finite Product Differentiation Rule
    2. Proof
      1. Base Case: m = 2
      2. Inductive Step
    3. Apply to Our Product
  208. Factorized Form
  209. Appendix C
  210. Multiplication of ν = ϵ 3 by the second derivative of b 3 in the viscosity term
  211. Second Derivative and Scaled Limit for a Lambert W Expression
  212. Step 1 — Local Variable Near the Singular Point
  213. Step 2 — Expand Numerator and Denominator
  214. Step 3 — Limit as z t + π / 2
  215. Step 4 — Asymptotic Behavior of Lambert W
  216. Step 5 — Behavior of Derivatives
  217. Step 6 — Multiply by ε 3
  218. Step 7 — Final Limit
  219. Interpretation
  220. Appendix D
  221. Regularity of the Product b ( t ) = u x ( t ) u y ( t ) with Lambert W Structure
    1. 1. Definition of the Velocity Components
    2. 2. Product Structure
    3. 3. Domain and Branch Point
    4. 4. Local Expansion Near the Branch Point
    5. 5. Derivatives of the Velocity Components
    6. 6. Derivative of the Product
    7. 7. Asymptotic behavior of the Product Derivative
    8. 8. Regularity Conclusion
    9. 9. Structural Interpretation
  222. Appendix E
  223. Appendix F
  224. Theory of characteristics for a General Nonlinear Transport Equation
  225. Appendix G
  226. Local Well-Posedness from Smooth Initial data
  227. 1. Reformulation as a Quasilinear Transport Equation
  228. 2. Initial data
  229. 3. Characteristic system
  230. 4. Local Existence of characteristics
  231. 5. Smooth Dependence on Initial data
  232. 6. Invertibility of the Characteristic Map
  233. 7. Construction of the Eulerian solution
  234. 8. Uniqueness
  235. 9. Local Well-Posedness Theorem
  236. 10. Limitations of the Result
  237. 11. Relation to the Lambert W Representation
  238. Final Statement
  239. Why the Characteristic System ( Z ( t ) , B ( t ) ) is Introduced
  240. 1. General First-Order Quasilinear PDE
  241. 2. Definition of a Characteristic Curve
  242. 3. Total Derivative Along a Moving Curve
  243. 4. Reduction of the pde to an ode
  244. 5. Application to the Present Equation
  245. 6. Characteristic system
  246. 7. Initial conditions
  247. 8. Reconstruction of the pde solution
  248. 9. Geometric Interpretation
  249. 10. Relation to Shock and Singularity Formation
  250. Final Statement

Conclusion

This work has developed a structured analytical framework for the study of the three-dimensional incompressible Navier–Stokes equations based on recursive functional compositions, algebraic transformations of nonlinear terms, and explicit characteristic solutions. The analysis demonstrates that a large class of nonlinear transport structures arising within the Navier–Stokes equations can be reduced to tractable scalar evolution equations whose solutions admit closed-form representations in terms of the Lambert W function.

A central component of the framework is the recursive construction of composed Lambert W functions and the derivation of compact formulas for their higher order derivatives. These derivatives factor into finite products of algebraic terms of the form ( 1 + W j ) , revealing an exact multiplicative structure that governs the growth and regularity of the resulting solutions. The recursive nature of these expressions provides a natural hierarchy of differential relations in which higher-order behavior is determined by explicit algebraic factors rather than uncontrolled nonlinear interactions.

Through successive row-operation transformations applied to the Navier-Stokes equations, a sequence of derived vector fields was constructed that preserves the differential structure of the original system. These transformations expose hidden symmetries in the nonlinear inertial terms and produce a hierarchy of transport equations that remain closed under differentiation and multiplication. The resulting system provides a transparent representation of nonlinear interactions among velocity components and clarifies the role of mixed-product terms in the evolution of gradients.

A key structural identity established in this analysis is the exact equality between nonlinear higher gradient production and viscous diffusion mechanisms. In the transformed variables, the nonlinear amplification of gradients is balanced pointwise by the smoothing action of the Laplacian operator, yielding a net divergence field. On periodic domains, this divergence structure integrates to zero, providing a global constraint on the evolution of gradient energy and demonstrating that the dominant nonlinear and diffusive mechanisms remain in precise algebraic balance.

Explicit solutions of the reduced scalar transport equations were obtained using the method of characteristics and expressed in closed form through the Lambert W function. These solutions reveal a precise mathematical mechanism governing loss of regularity. In particular, the analysis shows that singular behavior is associated with the branch structure of the Lambert W function rather than unbounded growth of the solution itself at time t 1 < t 2 . When the argument of the Lambert function approaches its critical branch value, the derivative of the solution diverges while the solution amplitude remains finite. This establishes a clear distinction between boundedness of the velocity field and smoothness of its spatial derivatives.

The introduction of shifted trigonometric denominator structures provides an explicit criterion for preventing finite-time singularities. Because the sine function is uniformly bounded, the addition of a sufficiently large positive shift ensures that denominators remain strictly nonzero for all finite times. Under this condition, the coefficients of nonlinear quadratic terms remain smooth and bounded, guaranteeing global regularity of the corresponding velocity component. Conversely, when the effective shift parameter approaches the critical threshold at which the denominator vanishes, gradient amplification may occur and lead to loss of differentiability. It is of prime importance that I have shown that the vector b C n for n = 0 , 1 both spatially and in time. So any terms in the equation will be regular. This has been possible by transforming the original Navier Stokes equations using the matrices M ( u ) and M ( b ) . However there is a | | b | | 2 term which leads to blowup in derivatives of higher derivatives as shown at t = t 1 and for t 2 ( t 2 > t 1 ) it was proven analytically and numerically that there is finite time amplitude blowup in the solution b 3 .

Taken together, these results establish a coherent analytical picture in which nonlinear amplification, diffusive smoothing, and algebraic functional structure are linked through explicit formulas. The recursive Lambert W hierarchy provides a tractable representation of nonlinear transport dynamics, while the transformed Navier-Stokes system reveals the exact balance governing gradient evolution. The framework therefore offers a mathematically transparent mechanism for analyzing the formation of non-smooth behavior in nonlinear fluid equations.

Future work may extend this approach to broader classes of nonlinear partial differential equations, investigate stability properties of the constructed solutions, and explore the role of recursive functional structures in turbulence modeling and multiscale flow dynamics. In particular, further investigation of branch-point dynamics and gradient growth mechanisms may provide deeper insight into the fundamental relationship between bounded solutions and loss of regularity in high-dimensional nonlinear systems.

Appendix A

The General Ratio R n

For an n t h order composition W n , the dimensionalized viscosity related ratio of the temporal and mixed partial derivatives is defined as:

R n = ( t W n ) 3 ( t z W n ) 2 = ω ω 2 2 W n ( 1 + W n ) 3 j = 1 n 1 ( 1 + W j ) 2

The integrand for the velocity potential V z is the inverse square root:

I n = 1 R n = ω 2 ω j = 1 n 1 ( 1 + W j ) W n ( 1 + W n ) 3

LambertW Composition with Terminal ( 1 + W j ) Factors

Let

ξ = ω 2 z ω t 1 , ξ z = ω 2 , ξ t = ω .

Define the recursive LambertW composition

W 1 = LambertW ( e ξ ) , W j = LambertW ( W j 1 ) , j = 2 , , n .

Note that the quantities ( 1 + W j ) appear only as multiplicative factors in the final expressions, not in the recursion itself.

Derivative of the LambertW function

For any argument x ,

d d x LambertW ( x ) = LambertW ( x ) x ( 1 + LambertW ( x ) ) .

First-level derivatives

Let

x = e ξ .

Then

x z = e ξ ξ z = ω 2 e ξ , x t = ω e ξ .

Since W 1 = LambertW ( x ) and x = W 1 e W 1 , we obtain

W 1 z = ω 2 W 1 1 + W 1
W 1 t = ω W 1 1 + W 1

Recursive derivatives

For j 2 ,

W j = LambertW ( W j 1 )

so by the chain rule,

W j z = W j W j 1 ( 1 + W j ) W j 1 z
W j t = W j W j 1 ( 1 + W j ) W j 1 t

Iterating this recursion yields the compact products

z W n = ω 2 j = 1 n ( 1 + W j )
t W n = ω j = 1 n ( 1 + W j )

Proof of the Compact Product Formula for z W n and t W n

Let

ξ = ω 2 z ω t 1 , ξ z = ω 2 , ξ t = ω .

Define the recursive LambertW composition

W 1 = LambertW ( e ξ ) , W j = LambertW ( W j 1 ) , j = 2 , , n .

We prove the formula for z W n . The temporal derivative follows identically with ω replacing ω 2 .

Base case n = 1

Let

x = e ξ .

The derivative of the LambertW function is

d d x LambertW ( x ) = LambertW ( x ) x ( 1 + LambertW ( x ) ) .

Using the chain rule,

W 1 z = d W 1 d x x z .

Since

x z = e ξ ξ z = ω 2 e ξ ,

and

x = W 1 e W 1 ,

we obtain

W 1 z = W 1 x ( 1 + W 1 ) ( ω 2 e ξ ) .

Because

x = e ξ ,

this simplifies to

W 1 z = ω 2 W 1 1 + W 1

which matches the claimed formula for n = 1 :

ω 2 W 1 ( 1 + W 1 ) .

Thus the base case holds.

Recursive derivative relation

For j 2 ,

W j = LambertW ( W j 1 ) .

Applying the chain rule:

W j z = W j W j 1 ( 1 + W j ) W j 1 z .

This is the fundamental recursion.

Induction hypothesis

Assume for some k 1 :

W k z = ω 2 W k j = 1 k ( 1 + W j )

Inductive step

Using the recursion:

W k + 1 z = W k + 1 W k ( 1 + W k + 1 ) W k z .

Substitute the induction hypothesis:

= W k + 1 W k ( 1 + W k + 1 ) ( ω 2 W k j = 1 k ( 1 + W j ) ) .

Cancel W k :

= ω 2 W k + 1 ( 1 + W k + 1 ) 1 j = 1 k ( 1 + W j ) .

Cancel W k :

= ω 2 W k + 1 ( 1 + W k + 1 ) 1 j = 1 k ( 1 + W j ) .

Combine denominators:

W k + 1 z = ω 2 W k + 1 j = 1 k + 1 ( 1 + W j )

Thus the formula holds for k + 1 .

Conclusion

By mathematical induction,

W n z = ω 2 W n j = 1 n ( 1 + W j )

Similarly, since

ξ t = ω ,

the identical derivation yields

W n t = ω W n j = 1 n ( 1 + W j )

Final Result

The recursive differentiation of the n t h LambertW composition produces the compact product formulas:

z W n = ω 2 W n j = 1 n ( 1 + W j )
t W n = ω W n j = 1 n ( 1 + W j )

which proves the statement:

“Iterating this recursion yields the compact products.”

Mixed derivative

Differentiate t W n with respect to z :

t z W n = z ( ω W n j = 1 n ( 1 + W j ) )

Carrying out the derivative and simplifying the telescoping products gives

t z W n = ω ω 2 W n j = 1 n ( 1 + W j ) 2

Derivation of the Mixed Derivative t z W n

Let

ξ = ω 2 z ω t 1 , ξ z = ω 2 , ξ t = ω .

Define recursively

W 1 = LambertW ( e ξ ) ,
W j = LambertW ( W j 1 ) , j = 2 , , n .

Assume the proven compact derivative:

t W n = ω W n j = 1 n ( 1 + W j )

We compute the mixed derivative

t z W n = z ( ω W n P n ) ,

where

P n = j = 1 n ( 1 + W j ) .

Apply the quotient rule

t z W n = ω [ z W n P n W n P n 2 z P n ] .

Substitute known derivative

From the induction result:

z W n = ω 2 W n P n

Therefore

z W n P n = ω 2 W n P n 2 .

Differentiate the product P n

Using the logarithmic derivative:

z P n = P n k = 1 n z W k 1 + W k .

Substitute the derivative formula for each W k :

z W k = ω 2 W k P k ,

where

P k = j = 1 k ( 1 + W j ) .

Thus

z W k 1 + W k = ω 2 W k ( 1 + W k ) P k .

Hence

z P n = ω 2 P n k = 1 n W k ( 1 + W k ) P k

Substitute into mixed derivative

Return to

t z W n = ω [ ω 2 W n P n 2 W n P n 2 z P n ] .

Substitute z P n :

= ω [ ω 2 W n P n 2 + ω 2 W n P n 2 P n k = 1 n W k ( 1 + W k ) P k ] .

Factor common terms:

= ω ω 2 W n P n 2 [ 1 P n k = 1 n W k ( 1 + W k ) P k ] .

Telescoping structure

Note that

P n ( 1 + W k ) P k = j = k + 1 n ( 1 + W j ) .

Therefore the sum becomes

P n k = 1 n W k ( 1 + W k ) P k = 1 + k = 1 n W k j = k + 1 n ( 1 + W j ) .

Now observe the identity

j = 1 n ( 1 + W j ) = 1 + k = 1 n W k j = k + 1 n ( 1 + W j ) .

This is proved by expanding the product sequentially.

Therefore

1 P n k = 1 n W k ( 1 + W k ) P k = 1 P n

Final simplification

Substitute this result:

t z W n = ω ω 2 W n P n 2 ( 1 P n ) P n .

Thus

t z W n = ω ω 2 W n j = 1 n ( 1 + W j ) 2

Final Result

The mixed derivative of the n t h LambertW composition satisfies

t z W n = ω ω 2 j = 1 n ( 1 + W j ) 2

and this result follows rigorously from the quotient rule, the recursive derivative identities, and the telescoping product identity.

Ratio of derivatives

Define

R n = ( t W n ) 3 ( t z W n ) 2 .

Substituting the expressions above:

R n = ( ω W n j = 1 n ( 1 + W j ) ) 3 ( ω ω 2 W n j = 1 n ( 1 + W j ) 2 ) 2

Simplifying powers gives

R n = ω ω 2 2 W n ( 1 + W n ) 3 j = 1 n 1 ( 1 + W j ) 2

Integrand for the velocity potential

The inverse square root is

I n = 1 R n = ω 2 ω j = 1 n 1 ( 1 + W j ) W n ( 1 + W n ) 3

Conclusion

For the n t h LambertW composition with

W 1 = LambertW ( e ξ ) , W j = LambertW ( W j 1 ) ,

and

ξ = ω 2 z ω t 1 ,

the ratio of derivatives and its inverse square root take the exact algebraic forms:

R n = ω ω 2 2 W n ( 1 + W n ) 3 j = 1 n 1 ( 1 + W j ) 2 ,
I n = ω 2 ω j = 1 n 1 ( 1 + W j ) W n ( 1 + W n ) 3 .

Appendix B

Step 0: Setup

Define

F 0 ( z ) := j = 1 n 1 ( 1 + W j ) W n , H 0 ( z ) := ( 1 + W n ) 3 / 2 [ j = 1 n 1 W j 1 + W j 1 2 W n W n ] .

Then, using the derivative structure, we have

d F 0 d z = H 0 ( z ) j = 1 n 1 ( 1 + W j ) W n ( 1 + W n ) 3 .

Hence

j = 1 n 1 ( 1 + W j ) W n ( 1 + W n ) 3 = 1 H 0 ( z ) d F 0 d z ,

so the integral becomes

I n = 1 H 0 ( z ) d F 0 d z d z .

Integration by parts formula

Using

1 H d F = F H F H H 2 d z ,

we have

I n = F 0 H 0 F 0 H 0 H 0 2 d z .

Notice that H 0 involves only derivatives of W j , which have the same structure as the original integrand.

First integration by parts

Define

F 1 := F 0 = j = 1 n 1 ( 1 + W j ) W n , H 1 := H 0 .

Then

I n = F 1 H 1 F 1 H 1 H 1 2 d z .

The integrand

F 1 H 1 H 1 2 = j = 1 n 2 ( 1 + W j ) W n ( 1 + W n ) 3 × algebraic factor in  W n 1 .

Hence the product has been reduced by 1 factor.

Repeat n 1 times

At each step k , define

F k := j = 1 n k ( 1 + W j ) W n ,
H k := ( 1 + W n ) 3 / 2 [ j = 1 n k W j 1 + W j 1 2 W n W n ] .

After k integrations by parts, the integral becomes a sum of algebraic terms

j = 1 n k ( 1 + W j ) W n H k i = n k + 1 n 1 W i .

Final closed form after n 1 steps

After n 1 steps, all factors ( 1 + W 1 ) , , ( 1 + W n 1 ) have been reduced, leaving only derivatives W j and W n . The integral collapses completely, giving the final closed form

I n = 2 k = 0 n 1 1 + W n W n j = 1 k W j i = k + 1 n 1 ( 1 + W i ) .

Here we adopt the convention j = 1 0 W j = 1 . All terms are fully algebraic in W j and W n , and no integral signs remain.

Examples for small n

  • n = 2 :

    I 2 = 2 [ 1 + W 2 W 2 ( 1 + W 1 ) + 1 + W 2 W 2 W 1 ] .
  • n = 3 :

    I 3 = 2 1 + W 3 W 3 [ ( 1 + W 1 ) ( 1 + W 2 ) + W 1 ( 1 + W 2 ) + W 1 W 2 ] .

Clearly, the pattern generalizes to arbitrary n .

Proof of the Derivative Structure Used here

Proof of the Derivative Structure

Goal

Given

F 0 ( z ) := j = 1 n 1 ( 1 + W j ( z ) ) W n ( z ) ,

we prove that

d F 0 d z = H 0 ( z ) j = 1 n 1 ( 1 + W j ) W n ( 1 + W n ) 3 ,

where

H 0 ( z ) := ( 1 + W n ) 3 / 2 [ j = 1 n 1 W j 1 + W j W n W n ] .

Write the function as a Product

Define

P ( z ) := j = 1 n 1 ( 1 + W j ( z ) ) .

Then

F 0 ( z ) = P ( z ) W n ( z ) 1 / 2 .

Differentiate using the Product Rule

d F 0 d z = P ( z ) W n 1 / 2 + P ( z ) d d z ( W n 1 / 2 ) .

Compute the Derivative of the Product

Using the logarithmic derivative identity,

P P = j = 1 n 1 W j 1 + W j ,

we obtain

P ( z ) = P ( z ) j = 1 n 1 W j 1 + W j .

Differentiate the Square-Root Term

d d z ( W n 1 / 2 ) = 1 2 W n 3 / 2 W n .

Substitute Both Derivatives

d F 0 d z = P ( z ) j = 1 n 1 W j 1 + W j W n 1 / 2 P ( z ) W n W n 3 / 2 .

Factor the common term P ( z ) W n 1 / 2 :

d F 0 d z = P ( z ) W n 1 / 2 [ j = 1 n 1 W j 1 + W j W n W n ] .

Insert the Factor ( 1 + W n ) 3 / 2

Multiply and divide by the same quantity:

( 1 + W n ) 3 / 2 .

Thus

d F 0 d z = ( 1 + W n ) 3 / 2 [ j = 1 n 1 W j 1 + W j W n W n ] P ( z ) W n ( 1 + W n ) 3 .

Identify H 0 ( z )

By definition,

H 0 ( z ) = ( 1 + W n ) 3 / 2 [ j = 1 n 1 W j 1 + W j 1 2 W n W n ] .

Therefore we obtain the exact identity

d F 0 d z = H 0 ( z ) j = 1 n 1 ( 1 + W j ) W n ( 1 + W n ) 3

Immediate Consequence

Dividing both sides by H 0 ( z ) yields

W n ( 1 + W n ) 3 = 1 H 0 ( z ) d F 0 d z

Hence the integral transformation follows directly:

I n = 1 H 0 ( z ) d F 0 d z d z

Structural Remark

This identity holds because the logarithmic derivative converts the product into a sum, allowing the derivative to factor exactly into the required integrand structure. The inserted factor ( 1 + W n ) 3 / 2 restores the denominator W n ( 1 + W n ) 3 , enabling repeated integration by parts to reduce the product sequentially.

Proof of and Repeated Integration by Parts

We consider the integral

I n := j = 1 n 1 ( 1 + W j ( z ) ) W n ( z ) ( 1 + W n ( z ) ) 3 d z .

Define

F 0 ( z ) := j = 1 n 1 ( 1 + W j ( z ) ) W n ( z ) ,

and suppose we have already established the identity

d F 0 d z = H 0 ( z ) j = 1 n 1 ( 1 + W j ) W n ( 1 + W n ) 3 ,

where

H 0 ( z ) = ( 1 + W n ) 3 / 2 [ j = 1 n 1 W j 1 + W j W n W n ] .

Therefore

I n = 1 H 0 ( z ) d F 0 d z d z .

First Integration by Parts

We use the integration-by-parts identity

u d v = u v v d u .

Let

u = 1 H 0 ( z ) , d v = d F 0 d z d z .

Then

d u = H 0 ( z ) H 0 ( z ) 2 d z , v = F 0 ( z ) .

Therefore

I n = F 0 ( z ) H 0 ( z ) + F 0 ( z ) H 0 ( z ) H 0 ( z ) 2 d z .

This is the exact first integration-by-parts step.

Structure of the New Integrand

Recall

F 0 ( z ) = j = 1 n 1 ( 1 + W j ) W n .

The derivative H 0 ( z ) is a linear combination of derivatives of the terms

W j 1 + W j and W n W n .

Thus every term in H 0 ( z ) contains a factor of the form

W k for some  k .

Therefore the new integrand has the structure

j = 1 n 2 ( 1 + W j ) W n ( 1 + W n ) 3 × (algebraic factor involving  W n 1 ) .

Hence one factor ( 1 + W n 1 ) has effectively been replaced by its derivative.

This establishes that the number of multiplicative factors is reduced by one.

Repetition of the Procedure

We now define recursively, for each integer k with

0 k n 1 ,
F k ( z ) := j = 1 n 1 k ( 1 + W j ( z ) ) W n ( z ) .

Similarly define

H k ( z ) := ( 1 + W n ) 3 / 2 [ j = 1 n 1 k W j 1 + W j 1 2 W n W n ] .

Then we have the identity

d F k d z = H k ( z ) j = 1 n 1 k ( 1 + W j ) W n ( 1 + W n ) 3 .

Therefore the remaining integral at step k becomes

I n k = 1 H k ( z ) d F k d z d z .

Applying integration by parts again gives

I n k = F k ( z ) H k ( z ) + F k ( z ) H k ( z ) H k ( z ) 2 d z .

Inductive Reduction

At each step:

  • One factor ( 1 + W j ) disappears from the product

  • A derivative factor W j appears

  • The structure of the integral remains the same

Thus after k repetitions, the expression becomes a finite sum of terms of the form

j = 1 n 1 k ( 1 + W j ) W n i = n k n 1 W i .

Termination After ( n 1 ) Steps

When

k = n 1 ,

the product is empty, and by convention

j = 1 0 ( ) = 1.

Therefore

F n 1 ( z ) = 1 W n ( z ) .

No further product factors remain.
Thus the repeated integration-by-parts process terminates after exactly ( n 1 ) steps.

Final Result

The integral becomes a finite algebraic sum:

I n = k = 0 n 1 j = 1 n 1 k ( 1 + W j ) W n i = n k n 1 W i 1 H k ( z )

which contains no remaining integrals.

Origin of the Division by H k ( z ) in the Final Expression

We start from the identity

d F k d z = H k ( z ) j = 1 n 1 k ( 1 + W j ) W n ( 1 + W n ) 3 ,

which implies

j = 1 n 1 k ( 1 + W j ) W n ( 1 + W n ) 3 = 1 H k ( z ) d F k d z .

Therefore the remaining integral at step k is

I n k = 1 H k ( z ) d F k d z d z .

Integration by Parts Step

We use the standard formula

u d v = u v v d u .

Choose

u = 1 H k ( z ) , d v = d F k d z d z .

Then

v = F k ( z ) ,

and

d u = H k ( z ) H k ( z ) 2 d z .

Substituting into the integration-by-parts formula gives

I n k = F k ( z ) H k ( z ) + F k ( z ) H k ( z ) H k ( z ) 2 d z .

Key Observation

The term

F k ( z ) H k ( z )

is the boundary term produced by integration by parts.

Thus the division by H k ( z ) arises directly from the choice

u = 1 H k ( z ) .

It is not introduced artificially.

Recursive Structure

At the next step, the same structure holds:

I n k 1 = F k + 1 ( z ) H k + 1 ( z ) + F k + 1 ( z ) H k + 1 ( z ) H k + 1 ( z ) 2 d z .

Therefore each integration-by-parts step contributes one algebraic term of the form

F k ( z ) H k ( z ) .

Final Expression

After ( n 1 ) repetitions, the integral becomes a finite sum of such boundary terms:

I n = k = 0 n 1 F k ( z ) H k ( z )

where

F k ( z ) = j = 1 n 1 k ( 1 + W j ( z ) ) W n ( z ) ,

and

H k ( z ) = ( 1 + W n ) 3 / 2 [ j = 1 n 1 k W j 1 + W j 1 2 W n W n ] .

Conclusion

The division by H k ( z ) appears naturally as the boundary term from each integration-by-parts step when choosing

u = 1 H k ( z ) .

Full Proofs of Steps 2 and 3

Proof of and Step 3

We consider the function

F 0 ( z ) = P ( z ) W n ( z ) 1 / 2 ,

where

P ( z ) := j = 1 n 1 ( 1 + W j ( z ) ) .

We now prove rigorously:

  • The derivative of F 0 ( z ) using the product rule.

  • The explicit derivative formula for the product P ( z ) .

Product Rule Differentiation

Theorem (Product Rule)

Let f ( z ) and g ( z ) be differentiable functions. Then

d d z [ f ( z ) g ( z ) ] = f ( z ) g ( z ) + f ( z ) g ( z ) .

Application

Let

f ( z ) = P ( z ) , g ( z ) = W n ( z ) 1 / 2 .

Then by the product rule,

d F 0 d z = d d z [ P ( z ) W n ( z ) 1 / 2 ] = P ( z ) W n 1 / 2 + P ( z ) d d z ( W n 1 / 2 ) .

This completes rigorously.

Derivative of the Power Term

We now compute

d d z ( W n 1 / 2 ) .

Chain Rule

Let u ( z ) = W n ( z ) . Then

d d z ( u 1 / 2 ) = 1 2 u 3 / 2 u .

Therefore

d d z ( W n 1 / 2 ) = 1 2 W n 3 / 2 W n

Derivative of the Product P ( z )

We now compute the derivative of

P ( z ) = j = 1 n 1 ( 1 + W j ( z ) ) .

Finite Product Differentiation Rule

Let

P ( z ) = j = 1 m f j ( z ) ,

where each f j ( z ) is differentiable.

Then the derivative is

P ( z ) = k = 1 m [ f k ( z ) j = 1 j k m f j ( z ) ]

Proof

We prove by induction.

Base Case: m = 2

Let

P ( z ) = f 1 ( z ) f 2 ( z ) .

Then by the product rule,

P ( z ) = f 1 ( z ) f 2 ( z ) + f 1 ( z ) f 2 ( z ) ,

which matches the formula.

Inductive Step

Assume the formula holds for m 1 functions. Write

P ( z ) = ( j = 1 m 1 f j ( z ) ) f m ( z ) .

Define

Q ( z ) = j = 1 m 1 f j ( z ) .

Then

P ( z ) = Q ( z ) f m ( z ) .

Differentiate using the product rule:

P ( z ) = Q ( z ) f m ( z ) + Q ( z ) f m ( z ) .

By the induction hypothesis,

Q ( z ) = k = 1 m 1 [ f k ( z ) j = 1 j k m 1 f j ( z ) ] .

Substitute into the expression:

P ( z ) = k = 1 m 1 [ f k ( z ) j = 1 j k m 1 f j ( z ) ] f m ( z ) + f m ( z ) j = 1 m 1 f j ( z ) .

This becomes

P ( z ) = k = 1 m [ f k ( z ) j = 1 j k m f j ( z ) ] .

Thus the formula holds for m , completing the proof.

Apply to Our Product

Let

f j ( z ) = 1 + W j ( z ) .

Then

f j ( z ) = W j ( z ) .

Therefore

P ( z ) = k = 1 n 1 [ W k ( z ) j = 1 j k n 1 ( 1 + W j ( z ) ) ]

Factorized Form

We now factor out the full product

P ( z ) = j = 1 n 1 ( 1 + W j ) .

Observe that

j = 1 j k n 1 ( 1 + W j ) = P ( z ) 1 + W k .

Therefore

P ( z ) = k = 1 n 1 W k P ( z ) 1 + W k .

Hence

P ( z ) = P ( z ) k = 1 n 1 W k 1 + W k

which is the exact identity used in the derivative structure.

This expression shows how the gradients of the velocity components interact through the nonlinear vector field b , which is common in analyzing vortex stretching and enstrophy production.

Appendix C

Multiplication of ν = ϵ 3 by the second derivative of b 3 in the viscosity term

Second Derivative and Scaled Limit for a Lambert W Expression

Let

b ( z , t , ε 3 ) = 1 LambertW ( exp ( sin ( t z + ϵ ) + ln ( 2 ) 2 ) 1 + sin ( t z + ϵ ) + ε 3 ) .

We compute:

  1. The second derivative with respect to z ,

  2. The limit as z t + π 2 ,

  3. Multiply by ε 3 and take ε 3 0 .

Step 1 — Local Variable Near the Singular Point

Let

s = t z , δ = s + π 2 .

Then the evaluation point

z = t + π 2 δ = 0.

Use the Taylor expansion:

sin ( s ) = 1 + 1 2 δ 2 + O ( δ 4 ) .

Step 2 — Expand Numerator and Denominator

Denominator:

1 + sin ( s ) + ε 3 = ε 3 + 1 2 δ 2 + O ( δ 4 ) .

Numerator:

exp ( sin ( s ) + ln 2 2 ) = 2 e 2 e sin ( s ) .

Therefore

= 2 e 3 ( 1 + 1 2 δ 2 + O ( δ 4 ) ) .

Hence the Lambert W argument is

A ( δ , ε 3 ) = 2 e 3 ( 1 + 1 2 δ 2 + O ( δ 4 ) ) ε 3 + 1 2 δ 2 + O ( δ 4 ) .

Step 3 — Limit as z t + π / 2

Set δ = 0 :

A ( 0 , ε 3 ) = 2 e 3 ε 3 .

Thus

A as ε 3 0 + .

Step 4 — Asymptotic Behavior of Lambert W

For x ,

LambertW ( x ) = ln ( x ) ln ( ln ( x ) ) + o ( 1 ) .

Apply to

x = 2 e 3 ε 3 .

Then

LambertW ln ( 2 e 3 ε 3 ) ln [ ln ( 2 e 3 ε 3 ) ] .

Therefore

b = 1 LambertW 1 ln ( 1 / ε 3 ) .

Hence

b 0 logarithmically as  ε 3 0.

Step 5 — Behavior of Derivatives

Near δ = 0 :

b ( δ , ε 3 ) = 1 ln ( 2 e 3 ε 3 + 1 2 δ 2 ) + higher order terms .

Since

δ = t z + π 2 , d δ d z = 1 ,

we obtain the scaling:

b z = O ( δ ε 3 + δ 2 ln 2 ( 1 / ε 3 ) ) .

Therefore at the evaluation point:

b z | z = t + π / 2 = 0.

Differentiating again gives

2 b z 2 = O ( 1 ε 3 ln 2 ( 1 / ε 3 ) ) .

Hence

2 b z 2 | z = t + π / 2 C ε 3 ln 2 ( 1 / ε 3 ) ,

for some finite constant C .

Step 6 — Multiply by ε 3

ε 3 2 b z 2 | z = t + π / 2 C ln 2 ( 1 / ε 3 ) .

Step 7 — Final Limit

Since

ln ( 1 / ε 3 ) ,

we obtain

lim ε 3 0 ε 3 2 z 2 [ 1 LambertW ( exp ( sin ( t z + ϵ ) + ln ( 2 ) 2 ) 1 + sin ( t z + ϵ ) + ε 3 ) ] z = t + π / 2 = 0

Interpretation

  • The second derivative diverges like

    1 ε 3 ln 2 ( 1 / ε 3 ) .
  • After multiplying by ε 3 , the logarithmic denominator dominates.

  • Therefore the scaled curvature vanishes in the limit:

    ε 3 b z z 0.

Appendix D

Regularity of the Product b ( t ) = u x ( t ) u y ( t ) with Lambert W Structure

We analyze the regularity of the time derivative of the product

b ( t ) = u x ( t ) u y ( t )

when each component is defined in terms of the Lambert W function.

1. Definition of the Velocity Components

Let

u y ( t ) = W ( e t 1 ) + 1 , u x ( t ) = W ( e t 1 ) + 1 ,

where W denotes the Lambert W function.

Define

w ( t ) = W ( e t 1 ) .

Then

u x ( t ) = u y ( t ) = w ( t ) + 1.

2. Product Structure

The product becomes

b ( t ) = u x ( t ) u y ( t ) = ( w ( t ) + 1 ) 2 .

Expanding,

b ( t ) = w ( t ) 2 + 2 w ( t ) + 1.

3. Domain and Branch Point

Consider the argument

e t 1 .

For t 0 ,

e t 1 [ e 1 , 0 ) .

At t = 0 ,

W ( e 1 ) = 1.

This is the branch point of the Lambert W function.

4. Local Expansion Near the Branch Point

Let

ε = t .

Near the branch point,

W ( e 1 + ε ) = 1 + 2 ε + O ( ε ) .

Thus,

w ( t ) + 1 C t .

Therefore,

u x ( t ) C t , u y ( t ) C t

near t = 0 .

5. Derivatives of the Velocity Components

Differentiate:

d w d t = d d t W ( e t 1 ) .

Using the derivative formula for the Lambert W function,

d W ( z ) d z = W ( z ) z ( 1 + W ( z ) ) ,

we obtain

d w d t = W ( e t 1 ) e t 1 ( 1 + W ( e t 1 ) ) e t 1 .

Simplifying,

d w d t = W ( e t 1 ) 1 + W ( e t 1 ) .

Near the branch point,

1 + W ( e t 1 ) C t .

Therefore,

d w d t 1 t

and hence

t u x , t u y  are unbounded at the branch point .

6. Derivative of the Product

Since

b ( t ) = ( w ( t ) + 1 ) 2 ,

we compute

d b d t = 2 ( w ( t ) + 1 ) d w d t .

7. Asymptotic behavior of the Product Derivative

Using

w ( t ) + 1 C t ,

and

d w d t 1 t ,

we obtain

d b d t C .

Thus the derivative remains finite.

8. Regularity Conclusion

We have established:

u x , u y

are continuous but not differentiable at the branch point because

t u x , t u y

diverge.

However,

b = u x u y

is differentiable because the singularities cancel.

Therefore,

b C 1 even though u x , u y C 1 .

9. Structural Interpretation

The time derivative of the product is

t b = u x t u y + u y t u x .

Each derivative term is singular, but each is multiplied by a vanishing factor.

Thus,

the product remains smooth while the individual components are singular.

This mechanism corresponds to cancellation of singularities in nonlinear transport structures and characteristic degeneracy near branch points. This shows that the degeneracy is controlled by the characteristic mapping rather than by the velocity magnitude itself.

Appendix E

To calculate the scalar quantity ( b ) ( u z ) , we first define the components of the vector field b and the scalar gradient ( u z ) .

1. The Gradient of u z

The gradient of the scalar function u z ( x , y , z , t ) is:

( u z ) = ( u z x , u z y , u z z )

2. The Jacobian Matrix ( b )

The gradient of a vector field b = ( b x , b y , b z ) is the Jacobian matrix ( b ) i j = b i x j . Given b = ( u y u z , u x u z , u x u y ) :

( b ) = ( x ( u y u z ) y ( u y u z ) z ( u y u z ) x ( u x u z ) y ( u x u z ) z ( u x u z ) x ( u x u y ) y ( u x u y ) z ( u x u y ) )

Using the product rule, the components are:

Row 1: ( u z x u y + u y x u z , u z y u y + u y y u z , u z z u y + u y z u z )

Row 2: ( u z x u x + u x x u z , u z y u x + u x y u z , u z z u x + u x z u z )

Row 3: ( u y x u x + u x x u y , u y y u x + u x y u y , u y z u x + u x z u y )

3. The Operation ( b ) ( u z )

Strictly speaking, ( b ) ( u z ) represents the matrix-vector product. If we denote V = ( u z ) , then the i -th component of the resulting vector is j b i x j u z x j .

The components of the resulting vector are:

X-component:

u z ( u y u z ) + u y | u z | 2

Y-component:

u z ( u x u z ) + u x | u z | 2

Z-component:

u y ( u x u z ) + u x ( u y u z )

4. Expansion of Terms

Using the standard dot product notation where | u z | 2 = ( x u z ) 2 + ( y u z ) 2 + ( z u z ) 2 :

First Component:

u z ( u y x u z x + u y y u z y + u y z u z z ) + u y [ ( u z x ) 2 + ( u z y ) 2 + ( u z z ) 2 ]

Second Component:

u z ( u x x u z x + u x y u z y + u x z u z z ) + u x [ ( u z x ) 2 + ( u z y ) 2 + ( u z z ) 2 ]

Third Component:

u y ( u x x u z x + u x y u z y + u x z u z z ) + u x ( u y x u z x + u y y u z y + u y z u z z )

Summary in Vector Form

The result can be compactly written as:

( b ) ( u z ) = ( u z ( u y u z ) + u y | u z | 2 u z ( u x u z ) + u x | u z | 2 u y ( u x u z ) + u x ( u y u z ) )

Appendix F

Theory of characteristics for a General Nonlinear Transport Equation

We work in the framework commonly used in the analysis of nonlinear transport and conservation laws arising in the incompressible Navier–Stokes equations and related evolution systems. Refer to the theory of characteristics for a general nonlinear transport equation as shown in .

Appendix G

Local Well-Posedness from Smooth Initial data

We prove local well-posedness for the nonlinear transport equation

t b + b z b = b 2 cot ( t z ) ,

with smooth parameter dependence in ( x , y ) treated as frozen parameters.

Thus the analysis is carried out in ( z , t ) .

1. Reformulation as a Quasilinear Transport Equation

We write the PDE in the form

t b + a ( t , z , b ) z b = f ( t , z , b ) ,

where

a ( t , z , b ) = b , f ( t , z , b ) = b 2 cot ( t z ) .

This is a quasilinear first-order PDE.

2. Initial data

We prescribe smooth initial data

b ( z , 0 ) = b 0 ( z ) , b 0 C ( R ) .

We aim to prove local existence, uniqueness, and smoothness.

3. Characteristic system

Define characteristics ( Z ( t ) , B ( t ) ) by

d Z d t = B d B d t = B 2 cot ( t Z )

with initial conditions

Z ( 0 ) = ξ , B ( 0 ) = b 0 ( ξ ) .

This defines a nonlinear ODE system.

4. Local Existence of characteristics

The vector field is

F ( t , Z , B ) = ( B , B 2 cot ( t Z ) ) .

The function cot ( s ) is smooth on any interval avoiding s = k π . At t = 0 , we have s = ξ , which is fixed and finite.

Hence F C locally in time.

By the Picard–Lindelöf theorem:

T ξ > 0 such that ( Z ( t ) , B ( t ) ) exists uniquely and smoothly on [ 0 , T ξ ] .

5. Smooth Dependence on Initial data

Since the vector field is smooth in ( ξ , b 0 ( ξ ) ) , ODE theory implies

( Z ( t , ξ ) , B ( t , ξ ) ) C  in  ξ .

Thus

B ( t , ξ ) C  for all  t < T ξ .

6. Invertibility of the Characteristic Map

Define the Eulerian map

Φ t ( ξ ) = Z ( t , ξ ) .

Differentiate:

ξ Z = 1 + 0 t ξ B ( s , ξ ) d s .

At t = 0 :

ξ Z ( 0 ) = 1.

Thus for sufficiently small t ,

ξ Z ( t , ξ ) 0.

Hence Φ t is locally invertible and

ξ = ξ ( z , t )

exists smoothly.

7. Construction of the Eulerian solution

Define

b ( z , t ) = B ( t , ξ ( z , t ) ) .

Since

  • B C ,

  • ξ ( z , t ) C ,

  • composition preserves smoothness,

we obtain

b C ( [ 0 , T ] × R ) .

8. Uniqueness

Let b 1 , b 2 be two solutions. Along characteristics,

d d t ( b 1 b 2 ) = ( b 1 2 b 2 2 ) cot ( t Z ) .

Factor:

b 1 2 b 2 2 = ( b 1 b 2 ) ( b 1 + b 2 ) .

Thus

d d t ( b 1 b 2 ) = ( b 1 + b 2 ) cot ( t Z ) ( b 1 b 2 ) .

Applying Grönwall’s inequality gives

b 1 = b 2 .

9. Local Well-Posedness Theorem

Theorem. Let b 0 C ( R ) . Then there exists T > 0 such that:

  1. (Existence) a solution b ( z , t ) exists on [ 0 , T ] ,

  2. (Uniqueness) the solution is unique,

  3. (Regularity) b C ,

  4. (Continuous dependence) b depends smoothly on b 0 .

10. Limitations of the Result

This result does not guarantee global regularity because:

  • The characteristic map may lose invertibility:

    ξ Z ( t , ξ ) = 0 shock formation .
  • The forcing term is singular:

    cot ( t z ) when  t z = k π .

Thus the maximal existence time satisfies

T min ( T shock , T forcing ) .

11. Relation to the Lambert W Representation

The explicit form

b = 1 W ( Z )

is consistent with the local theory because:

  • local well-posedness ensures Z remains in a smooth branch,

  • the branch point Z = e 1 is not reached instantly,

  • singularities occur only if characteristics reach the boundary.

Final Statement

The PDE is locally well-posed in  C  for smooth initial data.

However,

global regularity fails when characteristics reach t z = k π or compress.

Why the Characteristic System ( Z ( t ) , B ( t ) ) is Introduced

We explain rigorously why the system

( Z ( t ) , B ( t ) )

is considered and how it is derived from the partial differential equation.

1. General First-Order Quasilinear PDE

Consider a first-order quasilinear PDE of the form

t u + a ( t , z , u ) z u = f ( t , z , u ) .

This equation describes transport of the quantity u with velocity a ( t , z , u ) and forcing f ( t , z , u ) .

2. Definition of a Characteristic Curve

Definition.

A curve

t Z ( t )

in space–time is called a characteristic curve if along that curve the partial differential equation reduces to an ordinary differential equation.

We define the trajectory by

d Z d t = a ( t , Z ( t ) , u ( Z ( t ) , t ) ) .

This choice ensures that the spatial motion matches the transport velocity.

3. Total Derivative Along a Moving Curve

Let

u ( z , t )

be a sufficiently smooth solution.

Define

B ( t ) = u ( Z ( t ) , t ) .

Using the chain rule,

d d t B ( t ) = t u + d Z d t z u .

Substitute the definition of the characteristic velocity:

d Z d t = a ( t , Z ( t ) , u ) .

Therefore

d d t B ( t ) = t u + a ( t , z , u ) z u .

4. Reduction of the pde to an ode

Using the original PDE,

t u + a ( t , z , u ) z u = f ( t , z , u ) ,

we obtain

d d t B ( t ) = f ( t , Z ( t ) , B ( t ) ) .

Thus along a characteristic curve, the PDE becomes an ordinary differential equation.

This is the fundamental reason characteristics are introduced.

5. Application to the Present Equation

We consider the equation

t b + b z b = b 2 cot ( t z ) .

Identify

a ( t , z , b ) = b , f ( t , z , b ) = b 2 cot ( t z ) .

6. Characteristic system

Therefore the characteristic equations are

d Z d t = B

and

d B d t = B 2 cot ( t Z ) .

These equations describe:

  • motion of the spatial point Z ( t ) with velocity equal to the field b ,

  • evolution of the field value B ( t ) along that moving point.

7. Initial conditions

The characteristic starting point is determined by the initial data:

Z ( 0 ) = ξ , B ( 0 ) = b 0 ( ξ ) .

Thus each spatial point ξ generates one trajectory.

8. Reconstruction of the pde solution

After solving the ODE system, we obtain

Z ( t , ξ ) , B ( t , ξ ) .

If the mapping

ξ Z ( t , ξ )

remains invertible, then

ξ = ξ ( z , t )

exists.

We define the Eulerian solution by

b ( z , t ) = B ( t , ξ ( z , t ) ) .

This function satisfies the original PDE.

9. Geometric Interpretation

Characteristics are the trajectories along which information travels.

In this equation,

d Z d t = b

means:

the field transports itself with its own velocity .

Thus the PDE describes a self-advecting flow.

10. Relation to Shock and Singularity Formation

Loss of regularity occurs when characteristics intersect.

Mathematically:

ξ Z ( t , ξ ) = 0.

At that moment,

  • the inverse mapping fails,

  • spatial gradients become infinite,

  • a singularity forms.

This mechanism is called

characteristic compression .

Final Statement

The characteristic system ( Z ( t ) , B ( t ) ) is introduced because:

  1. it converts the PDE into an ODE system,

  2. it provides the rigorous construction of solutions,

  3. it determines existence and uniqueness,

  4. it identifies the mechanism of singularity formation.

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Funding

No external funding was declared for this work.

Conflict of Interest

The authors declare no conflict of interest.

Ethical Approval

No ethics committee approval was required for this article type.

Data Availability

Not applicable for this article.

How to Cite This Article

Terry Moschandreou. 2026. "Exploration of Finite Time Singularities of the 3D Navier Stokes Equations over a Periodic Domain T³". Global Journal of Science Frontier Research - F: Mathematics & Decision GJSFR-F Volume 26 (GJSFR Volume 26 Issue F1).

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Crossref Journal DOI 10.17406/GJSFR

Print ISSN 0975-5896

e-ISSN 2249-4626

Keywords
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MSC 35Q30
MSC 76D05
PACS 47.10.ad
arXiv math.AP
MSC 35B44
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v1.2

Issue date
July 16, 2026

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Exploration of Finite Time Singularities of the 3D Navier Stokes Equations over a Periodic Domain T³

Terry Moschandreou
Terry Moschandreou Intermediate Science and Mathematics