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arxiv: 2606.19731 · v1 · pith:66HDPLWJnew · submitted 2026-06-18 · ⚛️ physics.flu-dyn

Forcing-informed resolvent analysis: Identification of input-output relations in self-sustained flows

Pith reviewed 2026-06-26 16:01 UTC · model grok-4.3

classification ⚛️ physics.flu-dyn
keywords forcing-informed resolvent analysisself-sustained flowsinput-output relationsnonlinear forcingenergy transfer mapcylinder wakeboundary layer transition
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The pith

Forcing-informed resolvent analysis extracts forcing and response modes that match actual self-sustained flow fields by incorporating nonlinear forcing structures from data.

A machine-rendered reading of the paper's core claim, the machinery that carries it, and where it could break.

The paper develops a forcing-informed resolvent framework that modifies the standard resolvent operator to account for the actual spatiotemporal patterns of nonlinear terms acting as forcing around a mean flow. Bases for the input subspace (from forcing snapshots) and output subspace are estimated directly from simulation data, so the resulting modes and singular values align with the observed flow rather than idealized linear assumptions. This holds at frequencies where nonlinear amplification dominates. The same snapshots can build the linear operator itself, producing a fully data-driven version. The framework also yields a nonlinear energy transfer map that shows where each forcing mode adds or removes fluctuation energy in space.

Core claim

The forcing-informed resolvent operator is built by estimating basis vectors for the input subspace spanned by forcing snapshots and for the output subspace from simulation data. The extracted response modes are linear combinations of the output basis, forcing modes are linear combinations of the input basis, and the singular values equal the actual output amplitudes. These properties make the identified modes and gains consistent with the statistics of the underlying self-sustained flow, as shown on the Stuart-Landau oscillator, two-dimensional cylinder wake, and three-dimensional transitional boundary layer.

What carries the argument

The forcing-informed resolvent operator, constructed from estimated input and output subspace bases derived from nonlinear forcing and response snapshots.

If this is right

  • Extracted FI response and forcing modes remain consistent with the actual self-sustained flow fields.
  • Singular values of the FI resolvent operator equal the measured output amplitudes.
  • Forcing snapshots alone suffice to build the linear operator for a fully data-driven analysis.
  • The nonlinear energy transfer map locates spatial regions where each extracted forcing mode injects or removes fluctuation energy.

Where Pith is reading between the lines

These are editorial extensions of the paper, not claims the author makes directly.

  • The energy transfer map could be used to rank spatial regions by their contribution to sustaining the flow at each frequency.
  • The data-driven construction might reduce the need for an explicit mean-flow linearization when only snapshot data are available.
  • The approach could be tested on additional self-sustained flows such as bluff-body wakes or mixing layers to check whether the same consistency holds.
  • If the input subspace basis is truncated too aggressively, the recovered forcing modes may miss localized nonlinear structures that still affect the overall energy balance.

Load-bearing premise

Basis vectors estimated from a finite number of simulation snapshots accurately represent the relevant structures of the nonlinear terms that act as forcing.

What would settle it

If the modes and gains produced by the method on the cylinder wake at a nonlinear frequency fail to reproduce the dominant fluctuation structures seen in the original simulation data, the consistency claim is falsified.

Figures

Figures reproduced from arXiv: 2606.19731 by Kunihiko Taira, Soshi Kawai, Yuta Iwatani.

Figure 1
Figure 1. Figure 1: Schematic of workflow of the present forcing-informed (FI) resolvent analysis, shown for an example of a [PITH_FULL_IMAGE:figures/full_fig_p003_1.png] view at source ↗
Figure 2
Figure 2. Figure 2: Time trajectories of the state vector 𝑞 ′ (blue) and the nonlinear forcing vector 𝑓 ′ NL (orange) of the Stuart–Landau oscillator. (a) The first components 𝑞 ′ 1 and 𝑓 ′ NL,1 from the initial condition to the limit cycle oscillation (LCO) at 0 ≤ 𝑡 ≤ 120. (b) All components at 152 ≤ 𝑡 ≤ 161 in the LCO domain. Solid lines, the first components of 𝑞 ′ and 𝑓 ′ NL; dashed lines, the second components. proposed … view at source ↗
Figure 3
Figure 3. Figure 3: Results for the Stuart-Landau oscillator. ( [PITH_FULL_IMAGE:figures/full_fig_p014_3.png] view at source ↗
Figure 4
Figure 4. Figure 4: Time evolutions of ⟨𝑞 ′ , 𝑳𝑞 ′ ⟩ (solid blue line), ⟨𝑞 ′ , 𝑓 ′ NL⟩ (solid orange line), and their sum (solid green line), for the Stuart-Landau system. The dashed blue/orange line is the time-averaged energy supply/removal due to the linear/nonlinear mechanisms during the LCO, evaluated using the leading FI response 𝑞ˆ𝐺,1 and forcing modes ˆ𝑓𝐺,1. Finally, to assess the energy balance between the linear and… view at source ↗
Figure 5
Figure 5. Figure 5: Data-driven estimate of linear time-invariant operator [PITH_FULL_IMAGE:figures/full_fig_p016_5.png] view at source ↗
Figure 6
Figure 6. Figure 6: Leading gains (singular values 𝜎1) for 2D cylinder case, obtained from the fully data-driven 𝑮FDD (orange circle), semi-data-driven 𝑮SDD (blue triangle), and the ordinary resolvent operator 𝑹 (gray plus), along with the secondary leading gains of 𝜎2 (𝑮FDD)(orange cross). The square roots of the leading eigenvalues SPOD gains 𝑺qq(red cross) are also shown. FI resolvent operator, which holds at the harmonics… view at source ↗
Figure 7
Figure 7. Figure 7: Spatial distributions of the leading FI response and forcing modes in 2D cylinder wake extracted by the fully [PITH_FULL_IMAGE:figures/full_fig_p017_7.png] view at source ↗
Figure 8
Figure 8. Figure 8: Conventional resolvent modes obtained using [PITH_FULL_IMAGE:figures/full_fig_p017_8.png] view at source ↗
Figure 9
Figure 9. Figure 9: Phase evolutions of the FI (a) response and (b) forcing modes at 𝑆𝑡𝐾 , along with the (normalized) streamwise component of phase velocity of FI (c) response and (d) forcing modes. In (b), the black arrows indicate the direction of the movement of the FI forcing mode structure. Spatial distributions of −∇∠𝑞ˆ𝐺,𝑚𝑥 /∥∇∠𝑞ˆ𝐺,𝑚𝑥 ∥ and −∇∠ ˆ𝑓𝐺,𝑚𝑥 /∥∇∠ ˆ𝑓𝐺,𝑚𝑥 ∥ are shown in (c) and (d), respectively. The gray isoli… view at source ↗
Figure 10
Figure 10. Figure 10: Same as figure 7 but for semi-data-driven approach using 𝑮SDD. X 3.4 4.0 4.6 5.2 5.8 6.4 7.0 Z 3 2 1 0 0 0.05 0.1 Y [PITH_FULL_IMAGE:figures/full_fig_p019_10.png] view at source ↗
Figure 11
Figure 11. Figure 11: Topview of the instantaneous iso-surfaces of Q criterion [PITH_FULL_IMAGE:figures/full_fig_p019_11.png] view at source ↗
Figure 12
Figure 12. Figure 12: Late stage of H-type transition, visualized by iso-surfaces of Q criterion ( [PITH_FULL_IMAGE:figures/full_fig_p020_12.png] view at source ↗
Figure 13
Figure 13. Figure 13: Eigenvalues 𝜆𝑟 + i𝜆𝑖 of the estimated linear operator 𝑳data obtained using 𝑁POD = 10, 90, 170, 250: (a) overall view; (b) enlarged view near unstable eigenvalues. X Z Y m̂ x /∥m̂ x∥∞ m̂ y /∥m̂ y∥∞ m̂ z /∥m̂ z∥∞ −0.38 0.38 −0.07 0.07 −0.02 0.02 −0.07 0.07 0.0 2.0 0.0 2.0 Z Z 0.0 2.0 Z 4.8 4.8 4.8 3.5 3.5 3.5 X X X 0.1 0.1 0.1 Y Y Y [PITH_FULL_IMAGE:figures/full_fig_p021_13.png] view at source ↗
Figure 14
Figure 14. Figure 14: Isosurfaces of momentum components 𝑚ˆ for the most unstable eigenmodes of the H-type transitional boundary layer (𝜆𝑖/𝜔2𝐷 ≈ 3/2), computed from the data-driven linear operator 𝑳data with 𝑁pod = 90: (left) streamwise 𝑚ˆ 𝑥, (middle) wall-normal 𝑚ˆ 𝑦, (right) spanwise 𝑚ˆ 𝑧 momentum components. For visualization, the iso-surfaces are copied once in the spanwise direction. amplification mechanism is predominant… view at source ↗
Figure 15
Figure 15. Figure 15: Gains, 𝜎𝐺,1 and 𝜎𝐺,2, of the FI resolvent operator 𝑮FDD for the transition boundary layer case, compared with the square root of the leading SPOD gains 𝜆 1/2 1 (𝑺qq). X 3.5 4.0 4.5 4.8 Z 𝜔/𝜔2D = 1/2 q ̂ mx (FI resp.) (FI forc.) (NL. energy trans. map) f ̂ mx 𝓣mx 1 0 1 0 1 0 X ≈ 4.25 X ≈ 4.5 X 3.5 4.0 4.5 4.8 Z 𝜔/𝜔2D = 2 q ̂ mx f ̂ mx 𝓣mx 1 0 1 0 1 0 X ≈ 4.25 X ≈ 4.5 (𝑎) (𝑏) [PITH_FULL_IMAGE:figures/full_… view at source ↗
Figure 16
Figure 16. Figure 16: Results of FI resolvent analysis of transitional boundary layer for streamwise momentum component at ( [PITH_FULL_IMAGE:figures/full_fig_p022_16.png] view at source ↗
Figure 17
Figure 17. Figure 17: Input-output relations at 𝑋 ≈ 4.5 where a perpendicularly standing ring-like vortex (PSRV) is observed. Streamwise momentum component of the FI response and forcing modes at 𝜔/𝜔2𝐷 = 1/2 (left) and 2 (middle). Snapshots of streamwise momentum component of the output 𝑚 ′ 𝑥 and nonlinear forcing 𝑓 ′ 𝑚𝑥 (right). attenuates the energy at this region, whereas that at 𝜔/𝜔2𝐷 = 2 in [PITH_FULL_IMAGE:figures/full_… view at source ↗
Figure 18
Figure 18. Figure 18: Comparison between the eigenmode 𝑚𝑥 (global stability mode) of 𝑳data using 𝑁POD = 90 and nonlinear energy transfer map 𝑻𝑚𝑥 , for streamwise momentum component, at 𝜔/𝜔2𝐷 = 1/2 and 2. Eigenvalues 𝜆𝑟 + i𝜆𝑖 of 𝑳data indicate the stability of the corresponding eigenmodes. 2012], the positive nonlinear energy transfer near the wall suggests a possible connection between nonlinear, intense sweep motions under th… view at source ↗
Figure 19
Figure 19. Figure 19: Comparison between the present nonlinear energy transfer maps computed from the most dominant FI [PITH_FULL_IMAGE:figures/full_fig_p027_19.png] view at source ↗
read the original abstract

We present a forcing-informed (FI) resolvent analysis framework to identify input-output relations for statistically stationary self-sustained unsteady flows. The central idea of this method is to inform the resolvent operator about the spatiotemporal structures of the nonlinear terms that act as exogenous forcing with respect to the mean flow. To construct the FI resolvent operator, we estimate the basis vectors for the input subspace spanned by forcing snapshots and, similarly, for the output subspace, from simulation data. The extracted FI response and forcing modes are expressed through the estimated bases of the output and input subspaces, respectively, and the singular values of the FI resolvent operator correspond to the actual output amplitudes. These properties ensure that the extracted modes are consistent with the actual self-sustained flow fields. Additionally, the forcing snapshots can be used to construct the linear operator, enabling a fully data-driven FI resolvent analysis. The proposed framework is validated using the Stuart-Landau oscillator and demonstrated for a two-dimensional cylinder wake and a three-dimensional transitional boundary layer. We successfully identify the gains and the corresponding pairs of forcing and response modes, even at frequencies where the nonlinear amplification mechanism is crucial. Furthermore, leveraging the balance between the time-averaged energy amplification/attenuation by the linear operator and nonlinear forcing, we introduce a nonlinear energy transfer map that identifies the spatial domains where the extracted forcing mode injects or removes fluctuation energy, thereby providing key physical insight into the self-sustaining mechanisms.

Editorial analysis

A structured set of objections, weighed in public.

Desk editor's note, referee report, simulated authors' rebuttal, and a circularity audit. Tearing a paper down is the easy half of reading it; the pith above is the substance, this is the friction.

Referee Report

2 major / 1 minor

Summary. The manuscript introduces a forcing-informed (FI) resolvent analysis framework for statistically stationary self-sustained unsteady flows. It estimates bases for the input subspace (spanned by forcing snapshots) and output subspace from simulation data to construct an informed resolvent operator that incorporates the spatiotemporal structure of nonlinear terms acting as exogenous forcing. The extracted FI response and forcing modes are expressed via these bases, with the singular values asserted to equal actual output amplitudes, ensuring consistency with the self-sustained fields. A fully data-driven variant constructs the linear operator from the same snapshots; the framework is validated on the Stuart-Landau oscillator, 2D cylinder wake, and 3D transitional boundary layer, and includes a nonlinear energy transfer map based on time-averaged energy balance.

Significance. If the consistency properties and validation hold under scrutiny, the approach could provide a practical route to extract input-output relations and physical insight into nonlinear self-sustaining mechanisms where standard mean-flow resolvent analysis is insufficient. The multi-case demonstration and the energy-transfer map are potentially useful contributions if the data-dependence issues are resolved.

major comments (2)
  1. [Abstract and method description] The central consistency claim (singular values equal actual output amplitudes; modes consistent with self-sustained fields) rests on the estimated input/output subspace bases from finite snapshots accurately spanning the relevant nonlinear forcing structures. The abstract and method description do not quantify truncation or sampling error in these bases, nor demonstrate that the projected operator preserves the true energy balance between linear amplification and nonlinear forcing.
  2. [Validation cases and fully data-driven variant] In the fully data-driven variant (linear operator also built from the same forcing snapshots), subspace estimation errors propagate simultaneously into the operator and the forcing representation. This compounds the risk that the reported gains and modes are artifacts of the shared data rather than robust identifications; explicit robustness checks (e.g., convergence with snapshot count or cross-validation) are required.
minor comments (1)
  1. Notation for the estimated bases, projection operators, and how the FI resolvent is assembled should be made fully explicit (including any regularization or truncation thresholds) to allow independent reproduction.

Simulated Author's Rebuttal

2 responses · 0 unresolved

We thank the referee for their thoughtful and constructive report. We address each major comment below, indicating planned revisions to strengthen the manuscript.

read point-by-point responses
  1. Referee: [Abstract and method description] The central consistency claim (singular values equal actual output amplitudes; modes consistent with self-sustained fields) rests on the estimated input/output subspace bases from finite snapshots accurately spanning the relevant nonlinear forcing structures. The abstract and method description do not quantify truncation or sampling error in these bases, nor demonstrate that the projected operator preserves the true energy balance between linear amplification and nonlinear forcing.

    Authors: We agree that the abstract and method description do not explicitly quantify truncation or sampling errors from finite snapshots. In the revised manuscript we will expand the method section to discuss the approximation properties: as the snapshot count increases the estimated bases converge to the true forcing/response subspaces and the singular values recover the actual amplitudes. We will also add a brief demonstration on the Stuart-Landau oscillator showing preservation of the linear-nonlinear energy balance once the snapshot ensemble is sufficiently rich. These additions will be placed after the definition of the FI resolvent operator. revision: yes

  2. Referee: [Validation cases and fully data-driven variant] In the fully data-driven variant (linear operator also built from the same forcing snapshots), subspace estimation errors propagate simultaneously into the operator and the forcing representation. This compounds the risk that the reported gains and modes are artifacts of the shared data rather than robust identifications; explicit robustness checks (e.g., convergence with snapshot count or cross-validation) are required.

    Authors: The concern about compounded data dependence in the fully data-driven variant is valid. Although the Stuart-Landau and cylinder-wake validations already compare against known reference solutions, we will add an explicit robustness subsection. This will include (i) convergence of the leading gains and modes versus snapshot count for the cylinder wake and (ii) a simple cross-validation by partitioning the snapshot set. These checks will be reported for both the standard and fully data-driven FI operators. revision: yes

Circularity Check

1 steps flagged

Subspace bases fitted to simulation snapshots force singular values to match data amplitudes by construction

specific steps
  1. fitted input called prediction [Abstract]
    "To construct the FI resolvent operator, we estimate the basis vectors for the input subspace spanned by forcing snapshots and, similarly, for the output subspace, from simulation data. The extracted FI response and forcing modes are expressed through the estimated bases of the output and input subspaces, respectively, and the singular values of the FI resolvent operator correspond to the actual output amplitudes. These properties ensure that the extracted modes are consistent with the actual self-sustained flow fields."

    The bases are obtained by fitting to the identical simulation snapshots whose amplitudes are later declared to be recovered by the singular values. Because the FI operator is the projection of the (mean-flow or data-derived) linear operator onto these bases, its SVD singular values are algebraically forced to reproduce the projected amplitudes; the claimed 'correspondence' and 'consistency' therefore reduce to the fitting step rather than constituting an independent prediction.

full rationale

The paper estimates input/output subspace bases directly from the same simulation snapshots that supply the nonlinear forcing and fluctuation amplitudes. The FI resolvent is then formed by projection onto these bases, after which the paper states that its singular values equal the actual output amplitudes and that the resulting modes are consistent with the flow fields. This match holds by the linear-algebra construction of the reduced operator rather than by independent verification; the fully data-driven variant (linear operator also built from snapshots) inherits the same dependence. No self-citation chain or external uniqueness theorem is invoked, so the circularity is moderate and localized to the data-driven projection step.

Axiom & Free-Parameter Ledger

0 free parameters · 1 axioms · 0 invented entities

The framework rests on treating nonlinear terms as exogenous forcing to the mean flow and on the assumption that finite snapshots yield representative bases for the relevant subspaces; no free parameters or new entities are mentioned.

axioms (1)
  • domain assumption Nonlinear terms in the Navier-Stokes equations can be treated as exogenous forcing with respect to the mean flow for the purpose of input-output analysis.
    This is the foundational modeling choice that allows the resolvent operator to be informed by forcing structures.

pith-pipeline@v0.9.1-grok · 5804 in / 1211 out tokens · 26114 ms · 2026-06-26T16:01:53.017183+00:00 · methodology

discussion (0)

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Reference graph

Works this paper leans on

133 extracted references · 108 canonical work pages

  1. [1]

    2001 , publisher=

    Stability and transition in shear flows , author=. 2001 , publisher=

  2. [2]

    and Naudascher, E

    Rockwell, D. and Naudascher, E. Review—Self -Sustaining Oscillations of Flow Past Cavities. J. Fluids Eng. doi:10.1115/1.3448624

  3. [3]

    Singh, A. N. and Nair, V. , journal=. Effects of harmonic forcing on self-sustained oscillations in cavity flows at low. 2025 , publisher=

  4. [4]

    Lee, B. H. K. Self-sustained shock oscillations on airfoils at transonic speeds. Prog. Aerosp. Sci. doi:10.1016/S0376-0421(01)00003-3

  5. [5]

    and Yeh, C.-A

    Kojima, Y. and Yeh, C.-A. and Taira, K. and Kameda, M. Resolvent analysis on the origin of two-dimensional transonic buffet. J. Fluid Mech. doi:10.1017/jfm.2019.992

  6. [6]

    On a self-sustaining process in shear flows

    Waleffe, F. On a self-sustaining process in shear flows. Phys. Fluids. doi:10.1063/1.869185

  7. [7]

    Nonlinear mechanism of the self-sustaining process in the buffer and logarithmic layer of wall-bounded flows , author=. J. Fluid Mech. , volume=. 2021 , publisher=

  8. [8]

    and Asada, H

    Iwatani, Y. and Asada, H. and Yeh, C.-A and Taira, K. and Kawai, S. Identifying the Self-Sustaining Mechanisms of Transonic Airfoil Buffet with Resolvent Analysis. AIAA J. doi:10.2514/1.J062294

  9. [9]

    and Moin, P

    Jiménez, J. and Moin, P. The minimal flow unit in near-wall turbulence. J. Fluid Mech. doi:10.1017/S0022112091002033

  10. [10]

    and Gayme, D

    Liu, C. and Gayme, D. F. Structured input–output analysis of transitional wall-bounded flows. J. Fluid Mech. doi:10.1017/jfm.2021.762

  11. [11]

    McKeon, B. J. and Sharma, A. S. and Jacobi, I. Experimental manipulation of wall turbulence: a systems approach. Phys. Fluids

  12. [12]

    Ribeiro, J. H. M. and Yeh, C.-A. and Taira, K. Randomized resolvent analysis. Phys. Rev. Fluids. doi:10.1103/PhysRevFluids.5.033902

  13. [13]

    Journal of Fluid Mechanics , volume=

    Structured input--output analysis of compliant wall turbulence , author=. Journal of Fluid Mechanics , volume=. 2026 , publisher=

  14. [14]

    Hydrodynamic stability without eigenvalues

    Trefethen, L N and Trefethen, A E and Reddy, S C and Driscoll, T A. Hydrodynamic stability without eigenvalues. Science. doi:10.1126/science.261.5121.578

  15. [15]

    Componentwise energy amplification in channel flows

    Jovanović, M and Bamieh, Bassam. Componentwise energy amplification in channel flows. J. Fluid Mech. doi:10.1017/S0022112005004295

  16. [16]

    Journal of Fluid Mechanics , author =

    McKeon, B J and Sharma, A S. A critical-layer framework for turbulent pipe flow. J. Fluid Mech. doi:10.1017/S002211201000176X

  17. [17]

    From Bypass Transition to Flow Control and Data-Driven Turbulence Modeling: An Input–Output Viewpoint

    Jovanović, Mihailo R. From Bypass Transition to Flow Control and Data-Driven Turbulence Modeling: An Input–Output Viewpoint. Annu. Rev. Fluid Mech. doi:10.1146/annurev-fluid-010719-060244

  18. [18]

    and Kerswell, R

    Page, J. and Kerswell, R. R. K oopman mode expansions between simple invariant solutions. J. Fluid Mech. doi:10.1017/jfm.2019.686

  19. [19]

    A reduced-order model of three-dimensional unsteady flow in a cavity based on the resolvent operator

    Gómez, F and Blackburn, H M and Rudman, M and Sharma, A S and McKeon, B J. A reduced-order model of three-dimensional unsteady flow in a cavity based on the resolvent operator. J. Fluid Mech. doi:10.1017/jfm.2016.339

  20. [20]

    FFVHC - ACE : Fully automated C artesian-grid-based solver for compressible large-eddy simulation

    Asada, Hiroyuki and Tamaki, Yoshiharu and Takaki, Ryoji and Yumitori, Takaaki and Tamura, Shun and Hatanaka, Keita and Imai, Kazuhiro and Maeyama, Hirotaka and Kawai, Soshi. FFVHC - ACE : Fully automated C artesian-grid-based solver for compressible large-eddy simulation. AIAA J. doi:10.2514/1.j062593

  21. [21]

    Resolvent-analysis-based design of airfoil separation control

    Yeh, Chi-An and Taira, Kunihiko. Resolvent-analysis-based design of airfoil separation control. J. Fluid Mech. doi:10.1017/jfm.2019.163

  22. [22]

    and Iwatani, Y

    Fukami, K. and Iwatani, Y. and Maejima, S. and Asada, H. and Kawai, S. Compact representation of transonic airfoil buffet flows with observable-augmented machine learning. J. Fluid Mech. doi:10.1017/jfm.2025.10741

  23. [23]

    Machine learning for fluid mechanics , author=. Annu. Rev. Fluid Mech. , volume=. 2020 , publisher=

  24. [24]

    and Fukami, K

    Fukagata, K. and Fukami, K. Compressing fluid flows with nonlinear machine learning: mode decomposition, latent modeling, and flow control. Fluid Dyn. Res. doi:10.1088/1873-7005/ade8a2

  25. [25]

    Data-driven transient lift attenuation for extreme vortex gust--airfoil interactions , author=. J. Fluid Mech. , volume=. 2024 , publisher=

  26. [26]

    Deep learning to discover and predict dynamics on an inertial manifold , author =. Phys. Rev. E , volume =. 2020 , month =. doi:10.1103/PhysRevE.101.062209 , url =

  27. [27]

    Dynamics of a data-driven low-dimensional model of turbulent minimal C ouette flow

    Linot, Alec J and Graham, Michael D. Dynamics of a data-driven low-dimensional model of turbulent minimal C ouette flow. J. Fluid Mech. doi:10.1017/jfm.2023.720

  28. [28]

    Exact coherent structures in two-dimensional turbulence identified with convolutional autoencoders

    Page, Jacob and Holey, Joe and Brenner, Michael P and Kerswell, Rich R. Exact coherent structures in two-dimensional turbulence identified with convolutional autoencoders. J. Fluid Mech. doi:10.1017/jfm.2024.552

  29. [29]

    Page , author=

    Computation of simple invariant solutions in fluid turbulence with the aid of deep learning: J. Page , author=. Nonlinear dynamics , volume=. 2025 , publisher=

  30. [30]

    Nonlinear transient disturbance growth analysis for the compressible external flow and application to a flow around circular cylinder

    Taniguchi, Nobutaka and Ohmichi, Yuya and Suzuki, Kojiro. Nonlinear transient disturbance growth analysis for the compressible external flow and application to a flow around circular cylinder. J. Comput. Phys. doi:10.1016/j.jcp.2024.113374

  31. [31]

    Interpolatory input and output projections for flow control

    Herrmann, Benjamin and Baddoo, Peter J and Dawson, Scott T M and Semaan, Richard and Brunton, Steven L and McKeon, Beverley J. Interpolatory input and output projections for flow control. J. Fluid Mech. doi:10.1017/jfm.2023.680

  32. [32]

    and Lozano-Durán, A

    Towne, A. and Lozano-Durán, A. and Yang, X. Resolvent-based estimation of space–time flow statistics. J. Fluid Mech. doi:10.1017/jfm.2019.854

  33. [33]

    and Jung, J

    Martini, E. and Jung, J. and Cavalieri, A. V. G. and Jordan, P. and Towne, A. Resolvent-based tools for optimal estimation and control via the Wiener–Hopf formalism. J. Fluid Mech. doi:10.1017/jfm.2022.102

  34. [34]

    and Benton, S

    Yeh, C.-A. and Benton, S. I. and Taira, K. and Garmann, D. J. Resolvent analysis of an airfoil laminar separation bubble at Re=500000. Phys. Rev. Fluids. doi:10.1103/physrevfluids.5.083906

  35. [35]

    Physical Review E—Statistical, Nonlinear, and Soft Matter Physics , volume=

    Rapid path to transition via nonlinear localized optimal perturbations in a boundary-layer flow , author=. Physical Review E—Statistical, Nonlinear, and Soft Matter Physics , volume=. 2010 , publisher=

  36. [36]

    Physical review letters , volume=

    Using Nonlinear Transient Growth to Construct the Minimal Seed for Shear Flow Turbulence , author=. Physical review letters , volume=. 2010 , publisher=

  37. [37]

    Annual Review of Fluid Mechanics , author =

    Mezić, I. Analysis of Fluid Flows via Spectral Properties of the K oopman Operator. Annu. Rev. Fluid Mech. doi:10.1146/annurev-fluid-011212-140652

  38. [38]

    and Godavarthi, V

    Kim, Y. and Godavarthi, V. and Rolandi, L. V. and Klamo, J. T. and Taira, K. Influence of three-dimensionality on wake synchronisation of an oscillatory cylinder. J. Fluid Mech. doi:10.1017/jfm.2024.1079

  39. [39]

    doi:10.1016/j.compbiomed.2024.109162

    Ohmichi, Y. Variational mode decomposition–based nonstationary coherent structure analysis for spatiotemporal data. Aerosp. Sci. Technol. doi:10.1016/j.ast.2024.109162

  40. [40]

    and Nichols, J

    Jeun, J. and Nichols, J. W. and Jovanović, M. R. Input-output analysis of high-speed axisymmetric isothermal jet noise. Phys. Fluids. doi:10.1063/1.4946886

  41. [41]

    Ribeiro, J. H. M. and Taira, K. , year=. Triglobal resolvent-analysis-based control of separated flows around low-aspect-ratio wings , volume=. doi:10.1017/jfm.2024.580 , journal=

  42. [42]

    and Semeraro, O

    Lesshafft, L. and Semeraro, O. and Jaunet, V. and Cavalieri, A. V. G. and Jordan, P. Resolvent-based modeling of coherent wave packets in a turbulent jet. Phys. Rev. Fluids. doi:10.1103/PhysRevFluids.4.063901

  43. [43]

    Luhar, M and Sharma, A. S. and McKeon, B. J. Opposition control within the resolvent analysis framework. J. Fluid Mech. doi:10.1017/jfm.2014.209

  44. [44]

    and Kaszás, B

    Haller, G. and Kaszás, B. Data-driven linearization of dynamical systems. Nonlinear Dyn. doi:10.1007/s11071-024-10026-x

  45. [45]

    AIAA Journal55(12), 4013–4041 (2017)

    Taira, K. and Brunton, S. L. and Dawson, S. T. M. and Rowley, C. W. and Colonius, T. and McKeon, B. J. and Schmidt, O. T. and Gordeyev, S. and Theofilis, V. and Ukeiley, L. S. Modal Analysis of Fluid Flows: An Overview. AIAA J. doi:10.2514/1.J056060

  46. [46]

    and Taira, K

    Fukami, K. and Taira, K. Grasping extreme aerodynamics on a low-dimensional manifold. Nat. Commun. doi:10.1038/s41467-023-42213-6

  47. [47]

    and Hemati, M.S

    Taira, K. and Hemati, M.S. and Brunton, S. L. and Sun, Y. and Duraisamy, K. and Bagheri, S. and Dawson, S. T. M. and Yeh, C-A. Modal Analysis of Fluid Flows: Applications and Outlook. AIAA J. doi:10.2514/1.J058462

  48. [48]

    and Schmidt, O

    Sato, S. and Schmidt, O. T. , year=. Parametric reduced-order modelling and mode sensitivity of actuated cylinder flow from a matrix manifold perspective , volume=. doi:10.1017/jfm.2025.10733 , journal=

  49. [49]

    and Jovanović, M

    Zare, A. and Jovanović, M. R. and Georgiou, T. T. Colour of turbulence. J. Fluid Mech. doi:10.1017/jfm.2016.682

  50. [50]

    and Schmidt, O

    Towne, A. and Schmidt, O. T. and Colonius, T. Spectral proper orthogonal decomposition and its relationship to dynamic mode decomposition and resolvent analysis. J. Fluid Mech. doi:10.1017/jfm.2018.283

  51. [51]

    and Cossu, C

    Hwang, Y. and Cossu, C. Amplification of coherent streaks in the turbulent C ouette flow: an input–output analysis at low R eynolds number. J. Fluid Mech. doi:10.1017/s0022112009992151

  52. [52]

    and Semeraro, O

    Morra, P. and Semeraro, O. and Henningson, D. S. and Cossu, C. On the relevance of R eynolds stresses in resolvent analyses of turbulent wall-bounded flows. J. Fluid Mech. doi:10.1017/jfm.2019.196

  53. [53]

    and Nogueira, P

    Morra, P. and Nogueira, P. A. S. and Cavalieri, A. V G and Henningson, D. S. The colour of forcing statistics in resolvent analyses of turbulent channel flows. J. Fluid Mech. doi:10.1017/jfm.2020.802

  54. [54]

    Nogueira, P. A. S. and Morra, P. and Martini, E. and Cavalieri, A. V. G. and Henningson, D. S. Forcing statistics in resolvent analysis: application in minimal turbulent C ouette flow. J. Fluid Mech. doi:10.1017/jfm.2020.918

  55. [55]

    and Illingworth, S

    Symon, S. and Illingworth, S. J. and Marusic, I. Energy transfer in turbulent channel flows and implications for resolvent modelling. J. Fluid Mech. doi:10.1017/jfm.2020.929

  56. [56]

    and Rigas, G

    Pickering, E. and Rigas, G. and Schmidt, O. T. and Sipp, D and Colonius, T. Optimal eddy viscosity for resolvent-based models of coherent structures in turbulent jets. J. Fluid Mech. doi:10.1017/jfm.2021.232

  57. [57]

    Holford, J. J. and Lee, M. and Hwang, Y. Optimal white-noise stochastic forcing for linear models of turbulent channel flow. J. Fluid Mech. doi:10.1017/jfm.2023.234

  58. [58]

    and Kozul, M

    Fan, Y. and Kozul, M. and Li, W. and Sandberg, R. D. Eddy-viscosity-improved resolvent analysis of compressible turbulent boundary layers. J. Fluid Mech. doi:10.1017/jfm.2024.174

  59. [59]

    del Álamo, J. C. and Jiménez, J. Linear energy amplification in turbulent channels. J. Fluid Mech. doi:10.1017/S0022112006000607

  60. [60]

    and Symon, S

    Rosenberg, K. and Symon, S. and McKeon, B. J. Role of parasitic modes in nonlinear closure via the resolvent feedback loop. Phys. Rev. Fluids. doi:10.1103/PhysRevFluids.4.052601

  61. [61]

    and Zhu, X

    Barthel, B. and Zhu, X. and McKeon, B. Closing the loop: nonlinear T aylor vortex flow through the lens of resolvent analysis. J. Fluid Mech. doi:10.1017/jfm.2021.623

  62. [62]

    and Otto, S

    Padovan, A. and Otto, S. E. and Rowley, C. W. Analysis of amplification mechanisms and cross-frequency interactions in nonlinear flows via the harmonic resolvent. J. Fluid Mech. doi:10.1017/jfm.2020.497

  63. [63]

    and Rowley, C

    Padovan, A. and Rowley, C. W. Analysis of the dynamics of subharmonic flow structures via the harmonic resolvent: Application to vortex pairing in an axisymmetric jet. Phys. Rev. Fluids. doi:10.1103/PhysRevFluids.7.073903

  64. [64]

    and Sipp, D

    Rigas, G. and Sipp, D. and Colonius, Tim. Nonlinear input/output analysis: application to boundary layer transition. J. Fluid Mech. doi:10.1017/jfm.2020.982

  65. [65]

    Wereley, N. M. and Hall, S. R. Linear time periodic systems: Transfer function, poles, transmission zeroes and directional properties. 1991 American Control Conference. doi:10.23919/acc.1991.4791563

  66. [66]

    and He, G

    Wu, C and Zhang, X.-L. and He, G. Neural operator-based stochastic forcing for resolvent prediction of space–time turbulence statistics in channel flows. J. Fluid Mech. doi:10.1017/jfm.2025.10847

  67. [67]

    and Ying, A

    Chen, X. and Ying, A. and Gan, J. and Fu, L. Uncovering the forcing statistics in stochastic linear models for compressible wall-bounded turbulence. J. Fluid Mech. doi:10.1017/jfm.2025.10339

  68. [68]

    Kamal, O and Lakebrink, M. T. and Colonius, T. Global receptivity analysis: physically realizable input–output analysis. J. Fluid Mech. doi:10.1017/jfm.2023.48

  69. [69]

    and Sipp, D

    Leclercq, C. and Sipp, D. Mean resolvent operator of a statistically steady flow. J. Fluid Mech. doi:10.1017/jfm.2023.530

  70. [70]

    Space-time POD and the H ankel matrix

    Frame, P and Towne, A. Space-time POD and the H ankel matrix. PLoS One. doi:10.1371/journal.pone.0289637

  71. [71]

    , journal=

    Welch, P. , journal=. The use of fast. 2003 , publisher=

  72. [72]

    and Raveh, D

    Poplingher, L. and Raveh, D. E. and Dowell, E. H. Modal Analysis of Transonic Shock Buffet on 2D Airfoil. AIAA Journal. doi:10.2514/1.J057893

  73. [73]

    On dynamic mode decomposition: Theory and applications

    Tu, Jonathan H and Rowley, Clarence W and Luchtenburg, Dirk M and Brunton, Steven L and Kutz, J Nathan. On dynamic mode decomposition: Theory and applications. J. Comput. Dyn. doi:10.3934/jcd.2014.1.391

  74. [74]

    and Baddoo, P

    Herrmann, B. and Baddoo, P. J. and Semaan, R and Brunton, S. L. and McKeon, B. J. Data-driven resolvent analysis. J. Fluid Mech. doi:10.1017/jfm.2021.337

  75. [75]

    Exact parallelized dynamic mode decomposition with H ankel matrix for large-scale flow data

    Asada, H and Kawai, S. Exact parallelized dynamic mode decomposition with H ankel matrix for large-scale flow data. Theor. Comput. Fluid Dyn. doi:10.1007/s00162-024-00730-0

  76. [76]

    Turbulence and the dynamics of coherent structures

    Sirovich, L. Turbulence and the dynamics of coherent structures. I . Coherent structures. Quart. Appl. Math

  77. [77]

    Guide to spectral proper orthogonal decomposition

    Schmidt, O T and Colonius, T. Guide to spectral proper orthogonal decomposition. AIAA J

  78. [78]

    Schmid, P. J. Dynamic mode decomposition of numerical and experimental data. J. Fluid Mech. doi:10.1017/s0022112010001217

  79. [79]

    Detecting strange attractors in turbulence

    Takens, F. Detecting strange attractors in turbulence. Dynamical Systems and Turbulence, Warwick 1980. 1981

  80. [80]

    A mathematical example displaying features of turbulence

    Hopf, E. A mathematical example displaying features of turbulence. Commun. Pure Appl. Math. doi:10.1002/cpa.3160010401

Showing first 80 references.