Fuselage boundary-layer refraction of fan tones radiated from an installed turbofan aero-engine
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Each sheet of the spreadsheet corresponds to a figure in the paper. On each sheet is a table. In the table is numerical values used in the relevant figure. The units are in the top left of the table. The parameters are can be obtained from the paper. For the cylinder plots the azimuthal displacements is along the rows and the axial displacement is columns.
创建时间：
2017-02-10
