Steve Shkoller
· Professor of MathematicsVerifiedUniversity of California, Davis · Biomedical Engineering
Active 1994–2026
About
Professor Steve Shkoller is a mathematician whose research is extensively focused on the analysis of partial differential equations, fluid dynamics, and mathematical physics. His work encompasses a broad range of topics including the Euler and Navier-Stokes equations, compressible and incompressible fluid flows, free-boundary problems, shock formation, and the dynamics of interfaces in fluids. He has contributed to the rigorous mathematical understanding of complex phenomena such as shock waves, vorticity creation, and instabilities like Rayleigh-Taylor and Richtmyer-Meshkov. His research also addresses the well-posedness and stability of classical problems in fluid mechanics, including the Stefan problem and the Muskat problem, often involving sophisticated techniques in geometric analysis and nonlinear PDEs. Throughout his career, Professor Shkoller has collaborated with numerous researchers to develop new mathematical models and analytical methods for studying fluid interfaces, elastic solids interacting with fluids, and liquid crystal dynamics. His work includes the development of artificial viscosity methods for nonlinear conservation laws and the study of singularities in fluid flows. He has also contributed to the mathematical theory of Lagrangian averaged Euler and Navier-Stokes equations, providing insights into turbulence modeling and the geometry of diffeomorphism groups. His research has been supported by the National Science Foundation and published in leading journals, reflecting his significant impact on the field of mathematical fluid dynamics and applied analysis.
Research topics
- Mechanics
- Mathematics
- Mathematical analysis
- Physics
Selected publications
Sub-cell Wave Reconstruction from Differentiated Riemann Variables
SSRN Electronic Journal · 2026-01-01
preprintOpen access1st authorCorrespondingIntermittent Sub-grid Wave Correction from Differentiated Riemann Variables
SSRN Electronic Journal · 2026-01-01
preprintOpen access1st authorCorrespondingSub-cell Wave Reconstruction from Differentiated Riemann Variables
arXiv (Cornell University) · 2026-03-17
preprintOpen access1st authorCorrespondingWe introduce a postprocessing procedure that recovers sub-cell wave geometry from a standard one-dimensional Euler shock-capturing computation using differentiated Riemann variables (DRVs) -- characteristic derivatives that separate the three wave families into distinct localized spikes. Filtered DRV surrogates detect the waves, plateau sampling extracts the local states, and a pressure-wave-function Newton closure completes the geometry. The entire pipeline adds less than $0.25\%$ to the cost of a baseline WENO--5/HLLC solve. For Sod, a severe-expansion problem, and the LeBlanc shock tube, wave locations are recovered to within roundoff or $O(10^{-4})$ and the contact is sharpened to one cell width; a pattern-agnostic extension handles all four Riemann configurations with errors at the $10^{-6}$--$10^{-8}$ level. Direct comparison with MUSCL--THINC--BVD and WENO-Z--THINC--BVD shows that neither reproduces the combination of sharp contacts, small contact-window internal-energy error, and elimination of the LeBlanc positive overshoot achieved by the DRV reconstruction.
Incompressible Euler Blowup at the $C^{1,\frac{1}{3}}$ Threshold
ArXiv.org · 2026-03-11
articleOpen access1st authorCorrespondingWe prove finite-time Type-I blowup for the three-dimensional incompressible Euler equations in the axisymmetric no-swirl class, with initial velocity in $C^{1,α}(\mathbb{R}^3)\cap L^2(\mathbb{R}^3)$, odd symmetry in $z$, and $0<α<\tfrac13$, for an explicit class of finite-energy initial data. The singularity forms at a stagnation point on the symmetry axis. The on-axis axial strain and the global vorticity norm blow up at the Type-I rates $-\partial_z u_z(0,0,t)\sim (T^*-t)^{-1}$ and $\|ω(\cdot,t)\|_{L^\infty}\sim (T^*-t)^{-1}$, while the meridional Jacobian collapses according to $J(t)\sim (T^*-t)^{1/(1-3α)}$. The proof introduces a Lagrangian clock-and-strain framework that replaces the Eulerian self-similar ansatz used in prior work with a Lagrangian flow decomposition. The collapse dynamics are governed by a Riccati law for the on-axis axial strain, coupled to a clock ODE for the meridional Jacobian. The decisive step is a non-perturbative strain-pressure comparison showing that the pressure Hessian cannot cancel the quadratic compressive strain responsible for collapse. This gives a dynamical explanation of the threshold $α=\tfrac13$. The blowup mechanism is structurally stable and persists for an open set of admissible angular profiles in a weighted Hölder topology.
Intermittent Sub-grid Wave Correction from Differentiated Riemann Variables
arXiv (Cornell University) · 2026-03-23
articleOpen access1st authorCorrespondingWe introduce a low-cost every-$K$-step correction for one-dimensional Euler computations. The correction uses differentiated Riemann variables (DRVs) -- characteristic derivatives that isolate the left acoustic wave, the contact, and the right acoustic wave -- to locate the current wave packet, sample the surrounding constant states, perform a short Newton update for the intermediate pressure and contact speed, and conservatively remap a sharpened profile back onto the grid. The ingredients are elementary -- filtered centered differences, local state sampling, a single Newton step, and conservative cell averaging -- yet the effect on accuracy is disproportionate. On a long-time severe-expansion benchmark ($N=900$, $t=0.4$), intermittent correction drives the intermediate-state errors from $O(10^{-2})$ to $O(10^{-13})$, i.e. to machine precision. On a long-time LeBlanc benchmark ($N=800$, $t=1$), the method crosses a qualitative threshold: one-shot final-time reconstruction fails entirely (shock location error $2.7\times 10^{-1}$), whereas correction every three steps recovers an almost exact sharp solution with contact and shock positions accurate to machine precision. The same detector-and-Newton mechanism handles two-shock and two-rarefaction packets without case-specific logic, with plateau improvements of four to sixteen orders of magnitude. In an unoptimized Python prototype the wall-clock overhead is below a factor of two even on the most aggressively corrected benchmark. To our knowledge, no comparably lightweight fixed-grid add-on has been shown to recover this level of coarse-grid accuracy on the long-time LeBlanc and related near-vacuum problems.
Smooth and stable Euler implosions
arXiv (Cornell University) · 2026-05-01
preprintOpen accessWe construct a new class of self-similar implosion profiles for the multi-dimensional compressible Euler equations. These profiles are smooth, genuinely non-isentropic, radially/spherically symmetric, and have explicit (closed-form) similarity exponents. We prove that the exact Euler solution corresponding to the ground state implosion profile is stable to radially symmetric perturbations, as a solution to the full nonlinear compressible Euler equations, modulo a one-dimensional compatibility condition on the initial data. For perturbations of the Euler solution corresponding to the ground state implosion profile of a monatomic or diatomic gas, that do not obey any symmetry assumptions, we provide a complete characterization of the set of initial data that yield nonlinear stability.
Sub-cell Wave Reconstruction from Differentiated Riemann Variables
ArXiv.org · 2026-03-17
articleOpen access1st authorCorrespondingWe introduce a postprocessing procedure that recovers sub-cell wave geometry from a standard one-dimensional Euler shock-capturing computation using differentiated Riemann variables (DRVs) -- characteristic derivatives that separate the three wave families into distinct localized spikes. Filtered DRV surrogates detect the waves, plateau sampling extracts the local states, and a pressure-wave-function Newton closure completes the geometry. The entire pipeline adds less than $0.25\%$ to the cost of a baseline WENO--5/HLLC solve. For Sod, a severe-expansion problem, and the LeBlanc shock tube, wave locations are recovered to within roundoff or $O(10^{-4})$ and the contact is sharpened to one cell width; a pattern-agnostic extension handles all four Riemann configurations with errors at the $10^{-6}$--$10^{-8}$ level. Direct comparison with MUSCL--THINC--BVD and WENO-Z--THINC--BVD shows that neither reproduces the combination of sharp contacts, small contact-window internal-energy error, and elimination of the LeBlanc positive overshoot achieved by the DRV reconstruction.
Incompressible Euler Blowup at the $C^{1,\frac{1}{3}}$ Threshold
arXiv (Cornell University) · 2026-03-11
preprintOpen access1st authorCorrespondingWe prove finite-time Type-I blowup for the three-dimensional incompressible Euler equations in the axisymmetric no-swirl class, with initial velocity in $C^{1,α}(\mathbb{R}^3)\cap L^2(\mathbb{R}^3)$, odd symmetry in $z$, and $0<α<\tfrac13$, for an explicit class of finite-energy initial data. The singularity forms at a stagnation point on the symmetry axis. The on-axis axial strain and the global vorticity norm blow up at the Type-I rates $-\partial_z u_z(0,0,t)\sim (T^*-t)^{-1}$ and $\|ω(\cdot,t)\|_{L^\infty}\sim (T^*-t)^{-1}$, while the meridional Jacobian collapses according to $J(t)\sim (T^*-t)^{1/(1-3α)}$. The proof introduces a Lagrangian clock-and-strain framework that replaces the Eulerian self-similar ansatz used in prior work with a Lagrangian flow decomposition. The collapse dynamics are governed by a Riccati law for the on-axis axial strain, coupled to a clock ODE for the meridional Jacobian. The decisive step is a non-perturbative strain-pressure comparison showing that the pressure Hessian cannot cancel the quadratic compressive strain responsible for collapse. This gives a dynamical explanation of the threshold $α=\tfrac13$. The blowup mechanism is structurally stable and persists for an open set of admissible angular profiles in a weighted Hölder topology.
Smooth and stable Euler implosions
arXiv (Cornell University) · 2026-05-01
articleOpen accessWe construct a new class of self-similar implosion profiles for the multi-dimensional compressible Euler equations. These profiles are smooth, genuinely non-isentropic, radially/spherically symmetric, and have explicit (closed-form) similarity exponents. We prove that the exact Euler solution corresponding to the ground state implosion profile is stable to radially symmetric perturbations, as a solution to the full nonlinear compressible Euler equations, modulo a one-dimensional compatibility condition on the initial data. For perturbations of the Euler solution corresponding to the ground state implosion profile of a monatomic or diatomic gas, that do not obey any symmetry assumptions, we provide a complete characterization of the set of initial data that yield nonlinear stability.
Gradient catastrophes and an infinite hierarchy of Hölder cusp‐singularities for 1D Euler
Journal of the London Mathematical Society · 2025-08-01
articleAbstract We establish an infinite hierarchy of finite‐time gradient catastrophes for smooth solutions of the 1D Euler equations of gas dynamics with nonconstant entropy. Specifically, for all integers , we prove that there exist classical solutions, emanating from smooth, compressive, and nonvacuous initial data, which form cusp‐type gradient singularities in finite time, in which the gradient of the solution has precisely Hölder‐regularity. We show that such Euler solutions are codimension‐ stable in the Sobolev space .
Recent grants
Analysis of moving interface problems in fluid dynamics
NSF · $217k · 2013–2017
Well-posedness of moving interface problems in perfect fluids
NSF · $275k · 2010–2014
Well-posedness of moving interface problems in perfect fluids
NSF · $126k · 2007–2011
ITR: Analysis and Simulation of Interface Dynamics in Multiphase Fluids and Solids
NSF · $300k · 2003–2007
Frequent coauthors
- 48 shared
Daniel Coutand
- 29 shared
Vlad Vicol
- 20 shared
C. H. Arthur Cheng
National Central University
- 18 shared
Mahir Hadžić
- 17 shared
Jerrold E. Marsden
- 14 shared
Tristan Buckmaster
- 13 shared
Rafael Granero-Belinchón
- 7 shared
Tudor S. Raţiu
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