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NASA NTRS ยท 19910055333

Direct numerical study of crossflow instability

Abstract

Disturbances in the swept Hiemenz flow are calculated by solving the Navier-Stokes equations. The spatially-evolving base flow is treated exactly, allowing a check of the 'local' stability theories. Different types of disturbances such as random noise, waves, and wave packets, are input near the attachment line, develop in space, and exit through an outflow boundary. They all generate streamwise vortices. The effect of the Reynolds number, of the time-dependence of the noise, and of nonlinearity, are investigated.

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BibTeXRIS

Spalart, P. R.. 1990-01-01. Direct numerical study of crossflow instability. https://ntrs.nasa.gov/citations/19910055333

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