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Absolute instability in shock-containing jets

Fluid Dynamics · Submitted 23 Jun 2021

abstract compiled · 2026-09-23 · no language-model review

The authors' main claim The results suggest that screech can occur in the absence of a nozzle, and that the upstream reflection condition is not essential for screech frequency selection.

how it is stated · hedged possibility 1.00 read the record →

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arXiv ID2106.12690 (version 1)
Pith IDFRCO4WMZ, Pith's permanent record of this paper and its review
CitationAaron Towne, Andr\'e V. G. Cavalieri, Daniel Edgington-Mitchell, Peter Jordan, Petr\^onio A. S. Nogueira, Vincent Jaunet. "Absolute instability in shock-containing jets." arXiv:2106.12690 (2021). https://pith.science/paper/FRCO4WMZ
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The paper's own sentences, arranged. Each label is drawn from a closed vocabulary; the number beside it is the probability the classifier gave that label. Numbers in the tables are the authors', checked by code. No sentence in this record was written by a model.

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Compiled by classifier-1.13.0 via TypeSafe API, question bank abstract-p1-20260923, 2026-09-23: 1 request, 8,201 input tokens.

What the abstract itself states, as probabilities: claims first 0.04 · states limitation 0.25 · human participants 0.01 · controlled comparison 0.64 · randomized assignment 0.01 · states quantitative result 0.08 · compares with prior results 0.95 · mentions code or data availability 0.02.

The abstract, sentence by sentence

arXiv listing abstract v1. Results and the main claim are underlined; .

We present an analysis of the linear stability characteristics of shock-containing jets. The flow is linearised around a spatially periodic mean, which acts as a surrogate for a mean flow with a shock-cell structure, leading to a set of partial differential equations with periodic coefficients in space. Disturbances are written using the Floquet ansatz and Fourier modes in the streamwise direction, leading to an eigenvalue problem for the Floquet exponent. The characteristics of the solution are directly compared to the locally parallel case, and some of the features are similar. The inclusion of periodicity induces minor changes in the growth rate and phase velocity of the relevant modes for small shock amplitudes. On the other hand, the eigenfunctions are now subject to modulation related to the periodicity of the flow. Analysis of the spatio-temporal growth rates led to the identification of a saddle point between the Kelvin-Helmholtz mode and the guided jet mode, characterising an absolute instability mechanism. Frequencies and mode shapes related to the saddle points for two conditions (associated with axisymmetric and helical modes) are compared with screech frequencies and the most energetic coherent structures of screeching jets, resulting in a good agreement for both. The analysis shows that a periodic shock-cell structure has an impulse response that grows upstream, leading to oscillator behaviour. The results suggest that screech can occur in the absence of a nozzle, and that the upstream reflection condition is not essential for screech frequency selection. Connections to previous models are also discussed.

background contribution method result interpretation main claim

What the classifier reports for each sentence. The number is the probability it gave the label.
#sentencerolethe authors' own workstates the main conclusionstrength
s0 We present an analysis of the linear stability characteristics of shock-containing jets. contribution 1.00 0.94 0.03 asserted 0.87
s1 The flow is linearised around a spatially periodic mean, which acts as a surrogate for a mean flow with a shock-cell structure, leading to a set of partial differential equations with periodic coefficients in space. method 1.00 0.88 0.02 asserted 1.00
s2 Disturbances are written using the Floquet ansatz and Fourier modes in the streamwise direction, leading to an eigenvalue problem for the Floquet exponent. method 1.00 0.91 0.02 asserted 1.00
s3 The characteristics of the solution are directly compared to the locally parallel case, and some of the features are similar. result 0.94 0.86 0.03 asserted 0.96
s4 The inclusion of periodicity induces minor changes in the growth rate and phase velocity of the relevant modes for small shock amplitudes. result 1.00 0.91 0.04 asserted 1.00
s5 On the other hand, the eigenfunctions are now subject to modulation related to the periodicity of the flow. result 0.99 0.83 0.04 asserted 1.00
s6 Analysis of the spatio-temporal growth rates led to the identification of a saddle point between the Kelvin-Helmholtz mode and the guided jet mode, characterising an absolute instability mechanism. result 0.99 0.96 0.47 asserted 1.00
s7 Frequencies and mode shapes related to the saddle points for two conditions (associated with axisymmetric and helical modes) are compared with screech frequencies and the most energetic coherent structures of screeching jets, resulting in a good agreement for both. result 0.98 0.92 0.19 asserted 0.95
s8 The analysis shows that a periodic shock-cell structure has an impulse response that grows upstream, leading to oscillator behaviour. result 0.88 0.90 0.24 asserted 1.00
s9 The results suggest that screech can occur in the absence of a nozzle, and that the upstream reflection condition is not essential for screech frequency selection. interpretation 0.99 0.80 0.44 hedged possibility 1.00
s10 Connections to previous models are also discussed. background 0.47 0.48 0.02 unclear 0.71

What kind of paper the classifier reports this is: theoretical result 0.96 · evidence from proof or derivation 0.78.

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  • references and citing sentences
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Every quoted sentence on this record is the authors'. Every label is from Pith's closed vocabulary, with the probability shown beside it. Every number in the measurements table is the authors', checked by code. Record as JSON

The paper
Original abstract

We present an analysis of the linear stability characteristics of shock-containing jets. The flow is linearised around a spatially periodic mean, which acts as a surrogate for a mean flow with a shock-cell structure, leading to a set of partial differential equations with periodic coefficients in space. Disturbances are written using the Floquet ansatz and Fourier modes in the streamwise direction, leading to an eigenvalue problem for the Floquet exponent. The characteristics of the solution are directly compared to the locally parallel case, and some of the features are similar. The inclusion of periodicity induces minor changes in the growth rate and phase velocity of the relevant modes for small shock amplitudes. On the other hand, the eigenfunctions are now subject to modulation related to the periodicity of the flow. Analysis of the spatio-temporal growth rates led to the identification of a saddle point between the Kelvin-Helmholtz mode and the guided jet mode, characterising an absolute instability mechanism. Frequencies and mode shapes related to the saddle points for two conditions (associated with axisymmetric and helical modes) are compared with screech frequencies and the most energetic coherent structures of screeching jets, resulting in a good agreement for both. The analysis shows that a periodic shock-cell structure has an impulse response that grows upstream, leading to oscillator behaviour. The results suggest that screech can occur in the absence of a nozzle, and that the upstream reflection condition is not essential for screech frequency selection. Connections to previous models are also discussed.

Human review
How the literature uses it

2 arXiv papers cite this in 17 sentences

Each citing sentence is taken from the citing paper's LaTeX source and typed by Pith's classifier. A label appears at probability 0.8 or more (0.95 for support), a contest at 0.7 or more; the quoted words are the citing authors'. How each label was checked · JSON

Papers citing it · 13 sentences without a confident label

Builds on it 1 paper
  • This formulation builds upon the spatially periodic framework developed in [ref] ; here, the effect of the mean flow development can be directly estimated, providing a low-cost method for predicting the overall characteristics of the KH mode in these jets.

    Wavepacket modulation in shock-containing jets · Introduction · 0.91

Uses its method or tool 1 paper
Compares with it 1 paper
  • Figure [ref] shows sample eigenspectra for the present flow at $St=0.4$ and $0.7$, where similar features to [ref] are observed.

    Wavepacket modulation in shock-containing jets · Model problem: underexpanded $M_j=1.086$ jet · 0.96

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