Identification of all physical mechanisms responsible for the flow breakdown from laminar to
turbulent remains elusive in many high-speed boundary layer flows. Predicting the onset of …

In an aircraft, high-lift devices operating at high angle of attack promote the formation of
relatively large wakes. Such wakes influence the aerodynamic performance. The slat wake …

Sound generation in an asymmetric wake is studied by using a direct numeric solver for the
Navier-Stokes equations. This wake shares characteristics with both symmetrical wakes and …

O objetivo deste estudo é analisar a aeroacústica de esteiras assimétricas. Tal escoamento
pode ser encontrados a jusante de perfis aerodinãmicos que geram sustentação …

This paper presents a hybrid method for calculating sound generated by a mixing layer. The
method consists in calculating aerodynamic field through a Direct Numerical Simulation …

In an aircraft, high-lift devices operating at a high angle of attack promote the formation of
large wakes. Such wakes influence the aerodynamic performance. The slat wake, for …

ReP USP - Detalhe do registro: Method for aeroacoustic analysis in asymmetric wake flow
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