NASA NTRS · 19750004182
Analytical study of subsonic turbulent boundary layer separation including viscous-inviscid interaction
Abstract
The prediction of boundary layer deceleration and separation in regions of adverse pressure gradients are discussed as an unsolved problem of fundamental practical importance in aerodynamics. A three layered theoretical flow model of boundary layer separation including viscous-inviscid interaction was conceived for the case of subsonic two dimensional steady laminar flow.
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Inger, G. R.. 1974-11-30. Analytical study of subsonic turbulent boundary layer separation including viscous-inviscid interaction. https://ntrs.nasa.gov/citations/19750004182
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