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example_6.m
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example_6.m
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%% EXAMPLE 6: Calculate and plot confidence intervals for SPOD eigenvalues.
% The large-eddy simulation data provided along with this example is a
% subset of the database of a Mach 0.9 turbulent jet described in [1] and
% was calculated using the unstructured flow solver Charles developed at
% Cascade Technologies. If you are using the database in your research or
% teaching, please include explicit mention of Brès et al. [1]. The test
% database consists of 5000 snapshots of the symmetric component (m=0) of
% a round turbulent jet. A physical interpretaion of the SPOD results is
% given in [2], and a comprehensive discussion and derivation of SPOD and
% many of its properties can be found in [3].
%
% References:
% [1] G. A. Brès, P. Jordan, M. Le Rallic, V. Jaunet, A. V. G.
% Cavalieri, A. Towne, S. K. Lele, T. Colonius, O. T. Schmidt,
% Importance of the nozzle-exit boundary-layer state in subsonic
% turbulent jets, J. of Fluid Mech. 851, 83-124, 2018
% [2] Schmidt, O. T. and Towne, A. and Rigas, G. and Colonius, T. and
% Bres, G. A., Spectral analysis of jet turbulence, J. of Fluid Mech. 855, 953–982, 2018
% [3] Towne, A. and Schmidt, O. T. and Colonius, T., Spectral proper
% orthogonal decomposition and its relationship to dynamic mode
% decomposition and resolvent analysis, J. of Fluid Mech. 847, 821–867, 2018
%
% O. T. Schmidt ([email protected]), A. Towne, T. Colonius
% Last revision: 20-May-2020
clc, clear variables
addpath('utils')
disp('Loading the entire test database might take a second...')
load(fullfile('jet_data','jetLES.mat'),'p','x','r','dt');
%% SPOD with 99% confidence interval.
% This example is similar to example 3, but we also obtain the 99%
% confidence interval of the SPOD eigenvalues by calling
% [L,P,f,Lc] = SPOD(_) and specifying OPTS.conflvl.
opts.conflvl = 0.99; % return 99% confidence interval
% trapezoidal quadrature weights for cylindrical coordinates
intWeights = trapzWeightsPolar(r(:,1),x(1,:));
% SPOD using a retangular window of length 256 and 50 snaphots overlap
[L,P,f,Lc] = spod(p,ones(1,256),intWeights,50,dt,opts);
%% Plot the SPOD spectrum with upper and lower 99% confidence levels for every 5th mode.
figure
for mi = 1:5:size(L,2)
lh = loglog(f,L(:,mi),'LineWidth',1); hold on
loglog(f,Lc(:,mi,1),'LineWidth',0.1,'Color',get(lh,'Color'),'LineStyle','--'); % lower confidence level
loglog(f,Lc(:,mi,2),'LineWidth',0.1,'Color',get(lh,'Color'),'LineStyle','--'); % upper confidence level
end
set(gca,'XScale','log','YScale','log');
xlabel('frequency'), ylabel('SPOD mode energy')