2018
DOI: 10.2514/1.j057261
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Wind-Tunnel Investigation on the Compressive-Sensing Technique for Aeroengine Fan Noise Detection

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Cited by 26 publications
(8 citation statements)
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“…The inversion method itself, compared to the construction of forward models, is actually straightforward. To explain this point, the compressive sensing method is used here as an example, because it has found ever-increasing applications in aerospace engineering in general [38,39] and aeroengine acoustic experiments in particular [1][2][3]. Through compressive sensing, an inversion can be achieved by solving the following linear programming [40]:…”
Section: Preliminary Knowledge (A) Statement Of the Problemsmentioning
confidence: 99%
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“…The inversion method itself, compared to the construction of forward models, is actually straightforward. To explain this point, the compressive sensing method is used here as an example, because it has found ever-increasing applications in aerospace engineering in general [38,39] and aeroengine acoustic experiments in particular [1][2][3]. Through compressive sensing, an inversion can be achieved by solving the following linear programming [40]:…”
Section: Preliminary Knowledge (A) Statement Of the Problemsmentioning
confidence: 99%
“…Hence, the current paper is focused on the forward modelling topic. It is also worthwhile to mention that most fan noise testing techniques [1,2] currently used in aeroengine applications belong to mode detections, for which the transfer function G would simply be Fourier expansions (that mapŝ to azimuthal modes) or Bessel functions (that mapŝ to radial modes). In contrast, the mode inversion task calls for a transfer function G that maps fan noise source to far-field measurements, which would be much more difficult to achieve (figure 3) and is therefore one of the focal points in this work.…”
Section: Preliminary Knowledge (A) Statement Of the Problemsmentioning
confidence: 99%
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