Яндекс.Метрика

V.I. Zapryagaev, I.N. Kavun, I.I. Lipatov

Issue: 6 , Volume: 49 , Уear of publication: 2014
Serial edition: Fluid Dynamics
Pages: 819-826

Abstract

The results of an experimental and numerical investigation of a three-dimensional laminar separated flow in a compression corner are presented. The freestream Mach number M =6. The model under study is a plate with a sharp leading edge on which a step with a 30° inclination angle is mounted. The model width is equal to the plate length from the leading edge to the step. A thin high-pressure layer located above the boundary layer, downstream of the reattachment line is shown to exist
индекс в базе ИАЦ: 045488