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% subset of the database of a Mach 0.9 turbulent jet described in [1] and
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% was calculated using the unstructured flow solver Charles developed at
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% Cascade Technologies. If you are using the database in your research or
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% teaching, please include explicit mention of Brès et al. [1]. The test
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% teaching, please include explicit mention of Brès et al. [1]. The test
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% database consists of 5000 snapshots of the symmetric component (m=0) of
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% a round turbulent jet. A physical interpretaion of the SPOD results is
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% given in [2], and a comprehensive discussion and derivation of SPOD and
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% many of its properties can be found in [3].
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%
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% References:
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% [1] G. A. Brès, P. Jordan, M. Le Rallic, V. Jaunet, A. V. G.
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% [1] G. A. Brès, P. Jordan, M. Le Rallic, V. Jaunet, A. V. G.
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% Cavalieri, A. Towne, S. K. Lele, T. Colonius, O. T. Schmidt,
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% Importance of the nozzle-exit boundary-layer state in subsonic
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% turbulent jets, submitted to JFM, 2017
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% turbulent jets, J. of Fluid Mech. 851, 83-124, 2018
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% [2] Schmidt, O. T. and Towne, A. and Rigas, G. and Colonius, T. and
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% Bres, G. A., Spectral analysis of jet turbulence,
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% arXiv:1711.06296, 2017
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% Bres, G. A., Spectral analysis of jet turbulence, J. of Fluid Mech. 855, 953–982, 2018
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% [3] Towne, A. and Schmidt, O. T. and Colonius, T., Spectral proper
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% orthogonal decomposition and its relationship to dynamic mode
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% decomposition and resolvent analysis, arXiv:1708.04393, 2017
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% decomposition and resolvent analysis, J. of Fluid Mech. 847, 821–867, 2018
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%
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% O. T. Schmidt (oschmidt@caltech.edu), A. Towne, T. Colonius
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% Last revision: 5-Jan-2018
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% O. T. Schmidt (oschmidt@ucsd.edu), A. Towne, T. Colonius
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% Last revision: 20-May-2020
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clc, clear variables
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addpath('utils')
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% hard drive since we are in FFT saving mode (OPTS.savefft is true).
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figure
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loglog(f,L)
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xlabel('frequency'), ylabel('SPOD mode energy')
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xlabel('frequency'), ylabel('SPOD mode energy')

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