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The aforementioned problems of calculating the off-body induced velocity field and the pressure jump in the separated wake are thus avoided by disregarding the separation region and treating the separation streamlines bounding the separated wake as an extension of the displacement body streamline (as illustrated in Fig. 5).
An obvious disparity between the experimental data and that of the current method, which must be addressed, is that for mildly separated flows, it appears that the assumption of constant pressure in the separation region is not entirely realistic, and that there is in fact a slight pressure gradient in this region.
In essence, the separated wake is treated as an extension of the body surface, and the separation region is disregarded.
Fig. 6 Typical successive growth of separation region on aircraft.
The effect of mass transfer resistances on the separation region is analyzed.
The separation region provides a good mixing area for the injectant and the subsonic boundary layer.
The present paper focuses on the influence of AJVGs of various parameters on the separation region.
It is based on the lubrication approximation and simple physical notions regarding the separation region.
The presence of trailing vehicles was analyzed and the raising of the separation region evaluated.
Objectives include reduction in size of the separation region, surface loads and modulation of spectral content.
We observe that the separation region dimension leads to a higher degradation of efficiency in case of continuous busbar.
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Justyna Jupowicz-Kozak
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