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A complex mean flow develops in the gap and also behind the second cylinder.
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Statistical models for acoustic attenuation in non-uniform ducts with mean flow are developed.
A narrow shear zone of the zonal flow develops around the mixed layer top (where contour intervals of mean zonal flow are dense), and weak shear persists in the upper part of the mixed layer after the convective adjustment.
At intervals ranging from 20 to 40 months, with a mean value of 26 months, westerly winds in the stratosphere reverse direction over low latitudes, so that an easterly flow develops.
Formulae for the calculation of the sound fields generated by the interaction between a flat-plate semi-infinite aerofoil and a convected vortical gust in a supersonic mean flow have been developed in part 1.
Based on variations of the mean value and standard deviation of the thermal flow sensor signals, nine stages of unsteady flow developing events are identified with further evidence from flow visualization.
The flow developed and flow conditions were considered steady.
Expressions for the acoustic impedance under various mean flow and acoustic incidence configurations are developed.
A finite element simulation for propagation in non-uniform ducts with compressible mean flow with a random source description is developed.
To provide these profiles at all axial locations, a numerical scheme is developed to calculate the mean flow properties of a coaxial jet.
In this paper, a numerical scheme for modelling the straight-through resonator with mean flow based upon the boundary integral equation method is developed.
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