finite time blowup for navier–stokes · openai · 2026 · alternatives (c) and (d)
pages: core · pulse · stress · exterior · bands · solver · explorer
For every viscosity ν > 0 there is a smooth force, compactly supported in space and time, under which the three-dimensional incompressible Navier–Stokes equations, started from rest, have a smooth solution on [0, 1) whose velocity and pressure stay inside one fixed compact set, whose kinetic energy stays bounded — and whose maximum speed goes to infinity as t ↑ 1. Consequently no smooth solution with the same force and datum can exist for all time with bounded energy.
The paper is 166 pages, posted as a PDF by OpenAI with no named authors. This pack does not verify it. What it does is take the construction apart — a collapsing vortex, a ring of shear-fed pulses whose averaged momentum flux supplies the force the vortex is missing, and an exterior that is an exact heat flow — and implement each piece in the browser, with the paper's own formulas and exponents, so you can turn the knobs the proof fixes.
Fefferman's statement of the Millennium problem lists four alternatives and asks for a proof of any one of them. The two the paper claims are the forced breakdown ones. The unforced problem — smooth initial data, no force — is untouched.
| alternative | statement | status |
|---|---|---|
| (A) | Whole space ℝ³, no force: every smooth, decaying initial velocity gives a smooth global solution with bounded energy. | open |
| (B) | Periodic box 𝕋³, no force: same conclusion. | open |
| (C) | Whole space, with a smooth force: some smooth datum and force admit no smooth global solution with bounded energy. | claimed — Theorem 1.1, with zero initial datum |
| (D) | Periodic box, with a smooth force: same breakdown. | claimed — Corollary 10.6, by periodising the compactly supported fields |
The force is not a trick played on the equations: for any divergence-free u and pressure p, defining f as the residual ∂tu + (u·∇)u − ν∆u + ∇p makes Navier–Stokes hold by construction. The whole difficulty, and the whole paper, is choosing a flow that blows up while that residual — with every one of its derivatives — stays smooth through the singular time (§2).
A radial–axial section through the flow at time remaining τ = 1 − t. Three regions, each doing one job. Scrub τ to watch the core collapse onto the origin; switch to similarity units and the picture stops moving — that is what "self-similar" means.
Region radii Xa, Xb, Xc and the swirl shading are illustrative — the paper proves such radii exist and fixes them by estimates, it does not print them. The meridional arrows are exact for the paper's reference axis profile U = 4η (see core → meridional flow).
Viscosity is scaled out at the end: uν(x,t) = √ν·u(x/√ν, t) solves the equation at viscosity ν with force √ν·f(x/√ν, t) and the same singular time; energy scales by ν5/2 (10.22–10.23). The periodic case shrinks the support into a cube and sums integer translates, which never touch (Corollary 10.6).
Every scaling law against τ with h live; the similarity map q(z,τ); true meridional streamlines from the paper's axis profile; the viscosity and torus rescalings.
§2.1 · §3.1 · (4.7) · (10.22) /pulse/Integrates the wave-amplitude equation and overlays the envelope P(v); the exact Orr shearing wave; why vs > 2 is Rayleigh's centrifugal criterion with axial shear.
§7.1–7.2 · Lemma 7.4 · Craik–Criminale 1986 /stress/Reynolds stress from oscillations that average to nothing; the admissible stress cone drawn exactly from (ts, vs); drag the target and watch c₁, c₂.
§2.2 · §4.3 · Figure 4 · Proposition 7.5 /exterior/H(Z) by quadrature, K(r,τ), the pressure integral, the swirl heat equation's residual to machine precision, and a finite-difference solver checked against it.
(3.5) · (4.29) · (10.7) · Lemma A.6 /bands/Dyadic bands Q = 2−ℓ, ε = Qh, S* = ℓ²; carrier frequency, wavelength and amplitude ratios; the correction cycle; how small q must be before h = 1/100 does anything.
§3.6 · (6.1) · (7.2) · (9.8) /solver/Pseudo-spectral, hand-written FFT, runs in the tab. A shear-plus-wave experiment measures ⟨uv⟩ and the mean-flow feedback — the mechanism in its simplest setting — and shows why two dimensions cannot blow up.
contrast to §1 · Orr 1907 · Leray 1934 /explorer/A seeded, exactly divergence-free specimen of the leading-order field drawn live in WebGL: a section plane with pressure as colour and streaks of the meridional flow, spiralling streamlines, particles following the collapse, and the low-pressure core as a glow. Every seed is a permalink.
(3.2) · (4.5)–(4.7) · (4.25) · (4.29) · bismuth’s section trick| 1757 | Euler writes the inviscid equations. |
| 1822–45 | Navier, then Stokes, add the viscous term. |
| 1934 | Leray: global finite-energy weak solutions in 3D. Whether smooth data stay smooth is left open — the question ever since. |
| 1982 | Caffarelli–Kohn–Nirenberg: the singular set of a suitable weak solution has zero one-dimensional parabolic measure. Isolated singular points are not excluded. |
| 1986 | Craik–Criminale: exact finite-amplitude waves on affine shear flows — the wave's quadratic self-interaction cancels. The pulses here are their descendants. |
| 1991 | Lifschitz–Hameiri; Friedlander–Vishik: local instability criteria by following wavevectors along a background flow. |
| 2000 | Clay Mathematics Institute poses the problem; Fefferman's statement lists alternatives (A)–(D). |
| 2003 | Escauriaza–Seregin–Šverák: regularity under a bounded L∞tL³x norm. |
| 2016 | Tao: finite-time blowup for an averaged Navier–Stokes equation keeping the energy cancellation. |
| 2017–19 | Daneri–Székelyhidi (Euler), Buckmaster–Vicol (Navier–Stokes): convex integration — oscillations realise a prescribed stress; non-uniqueness of weak solutions. |
| 2022 | Albritton–Brué–Colombo: two distinct Leray–Hopf solutions from rest with the same (singular-in-time) force. |
| 2023–26 | Córdoba–Martínez-Zoroa (–Zheng): forced Euler blowup, then hypodissipative Navier–Stokes, by amplifying ever finer vortex layers while keeping the force smooth. |
| 2026 | This paper: full viscous Navier–Stokes, every ν > 0, smooth compactly supported force, bounded energy, unbounded velocity at t = 1. Claimed, unverified here. |
The official statement asks for a proof of any one of (A)–(D). The paper claims (C) and (D). Whether the argument holds is for referees and the community; a 166-page construction with a four-operation correction cycle iterated to infinite order is exactly the kind of thing that takes a long time to check. This site takes the paper at its word only about what it says, not about whether it is right.
No. The force is engineered: it is whatever residual the designed flow leaves behind, arranged so that residual is smooth. It says nothing about what a fluid does on its own from smooth initial data — alternatives (A) and (B) — and nothing about physical fluids, where the continuum model fails long before speeds become infinite.
The speeds diverge like τ−½−h on a core of volume τ3/2−h. Energy is speed squared times volume: τ1/2−3h, which tends to zero. Even the total dissipation ∫‖∇u‖² is finite, because its integrand ≍ τ−½−3h is integrable when h < 1/6. That is why the exponent is small.
Because individual terms of the momentum equation may diverge while their sum does not. The core balances itself to leading order; the annulus is balanced by the pulses' averaged momentum flux; the exterior is an exact solution; and everything left over is "flat" — every derivative is O(qN) for every N. Flat functions extend smoothly by zero, and Lemma 10.3 extends the force through t = 1 with the matching Taylor data.
It is the mismatch between radial and axial contraction, ℓz/ℓr ≍ τ−h. It makes axial diffusion weaker than radial diffusion by the factor q2h, which is the expansion parameter for the whole background correction series, and it gives the swirl Reynolds number Reθ ≍ τ−h → ∞ while the radial one stays O(1). The price is that q2h with h < 1/100 is only small when q is astronomically small — see bands.