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Research and mathematical modeling of turbulent boundary layer at positive pressure gradient... Presented mathematical model for the calculation of turbulent boundary layers and near-wall flows makes it possible to calculate such a complex and valuable from a practical point of view type of the flow as the aerodynamic trail behind the streamlined body.
général - core.ac.uk - PDF: doaj.org
Udc 629.735.083.02.06.(045) effect of hysteresis on efficiency of compressor cascades during streamlining by unsteady flows... Generalized results of research of hysteresis effect occurrence in aerodynamic perfor-mances of compressor cascades and its influence on compressor blade rings performances that operate in real conditions of periodic circular inlet distortion induced by aerodynamic trail behind the blade cascade of the compressor inlet guide vane are demonstrated

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industrie mécanique - techdico
transport terrestre - iate.europa.eu
transports aérien et spatial / environnement - iate.europa.eu
transports aérien et spatial / environnement - iate.europa.eu
transports aérien et spatial / environnement - iate.europa.eu
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