The Structure of Three-dimensional Separated Flows in Obstacle-boundary Layer Interactions

The Structure of Three-dimensional Separated Flows in Obstacle-boundary Layer Interactions
Author: Raymond Sedney
Publisher:
Total Pages: 64
Release: 1975
Genre: Boundary layer
ISBN:

The subject is investigated with flow visualization techniques; the turbulent boundary layer on the wall of a continuous supersonic wind tunnel is used. Sizeable separated flow regions can be studied since the wall width is 38cm and the boundary layer is typically 2.5cm thick. The large scale of the experiment is required to resolve the fine details of the flow structure. The flow visualization techniques are discussed. The structure of the separated flow upstream of the obstacle is seen to change with relatively small changes in Reynolds number R; the number of vortices varies from 6 to 4 to 2 as R changes. Data are presented for large and small protuberances, but the latter are emphasized.

Three-dimensional Separated Flow Topology

Three-dimensional Separated Flow Topology
Author: Jean Délery
Publisher: John Wiley & Sons
Total Pages: 181
Release: 2013-02-28
Genre: Science
ISBN: 1118579887

This book develops concepts and a methodology for a rational description of the organization of three-dimensional flows considering, in particular, the case where the flow is the place of separations. The descriptive analysis based on the critical point theory of Poincaré develops conventional but rather unfamiliar considerations from aerodynamicists, who face the understanding of complex flows including multiple separation lines and vortices. These problems concern industrial sectors where aerodynamics plays a key role, such as aerospace, ground vehicles, buildings, etc. Contents 1. Skin Friction Lines Pattern and Critical Points. 2. Separation Streamsurfaces and Vortex Structures. 3. Separated Flow on a Body. 4. Vortex Wake of Wings and Slender Bodies. 5. Separation Induced by an Obstacle or a Blunt Body. 6. Reconsideration of the Two-Dimensional Separation. 7. Concluding Remarks. About the Authors Jean Délery is a Supaero (French National Higher School of Aeronautics and Space) engineer who has worked at Onera (French national aerospace research center) since 1964. He has participated in several major French and European aerospace programs, is the author of many scientific publications, and has occupied various teaching positions particularly at Supaero, the University of Versailles-Saint-Quentin, Ecole polytechnique in France and “La Sapienza” University in Rome, Italy. He is currently emeritus adviser at Onera.

Boundary Layer Separation Due to 'Weak' and 'Strong' Viscous-Inviscid Interaction on an Inclined Body of Revolution

Boundary Layer Separation Due to 'Weak' and 'Strong' Viscous-Inviscid Interaction on an Inclined Body of Revolution
Author: H. U. Meier
Publisher:
Total Pages: 18
Release: 1984
Genre:
ISBN:

Detailed measurements in three-dimensional boundary layers and separated flow fields, developing on a prolate spheroid and flow visualizations are presented. The discussion is concentrated on the possible topological structure of separation patterns resulting from laminar on turbulent boundary layer flows at different Reynolds numbers. (Author).

Flow-visualization of Three-dimensional Boundary-layer Separation on Bodies of Revolution at Incidence

Flow-visualization of Three-dimensional Boundary-layer Separation on Bodies of Revolution at Incidence
Author: Taeyoung Han
Publisher:
Total Pages: 86
Release: 1977
Genre: Boundary layer
ISBN:

Surface streamline patterns on three bodies of revolution, namely a spheroid, a low-drag body and a hemisphere-hemispheroid combination body, have been examined at several angles of attack. Most of the tests were performed at low Reynolds numbers in a hydraulic flume using colored dye to make the surface flow visible. A limited number of experiments was also carried out in a wind tunnel, using wool tufts, to study the influence of Reynolds number and turbulent separation. The study has verified some of the important qualitative features of three-dimensional separation criteria proposed earlier by Maskell, Lighthill, Wang and others. The observed locations of laminar separation lines on a spheroid at various incidences have been compared with the numerical boundary-layer solutions of Wang, and it is suggested that the quantitative differences may be attributed to the significant viscous-inviscid interaction, especially at large incidences. (Author).