Abstract
A method is presented for calculating turbulent boundary layers with separation, reattachment, and viscousinviscid interaction. The boundary-layer method is a two-dimensional planar or axisymmetric inverse integral technique based on an analytical description of attached and separated turbulent boundary-layer velocity profiles. The inviscid region is calculated using a time-dependent, three-dimensional, finite-volume Euler equation code. Viscous-inviscid interaction is achieved using the surface source model. Transonic viscousinviscid interacting flows over planar, axisymmetric, and three-dimensional configurations are calculated and compared with experimental data.
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