The extensive interest in three-dimensional flow separation is linked closely with wings of high leading-edge sweep and bodies of large fineness ratio operating at large angles of incidence or yaw, that are typical of many high-speed aircraft and missile layouts. Characteristically, these boundary-layer separations can lead to comparatively steady streamwise vortrices, unlike the more familiar two-dimensional separations with their irregular mixing flows and buffeting. Customarily accompanying these strong viscous/inviscid interactins on hypersonic configurations is substantial heat transfer to the surface in zones of flow re-attachment. This part of the lecture series will deal with quasi-steady three-dimensional separated flows about practical flight vehicles. The general character of the three-dimensional attached boundary layer, separation and re-attachment will be offered. Specific examples will than be treated. (Stoehr)
Phenomenological aspects of quasi-stationary controlled and uncontrolled three-dimensional flow separations
Phaenomenologische Aspekte der quasistationaeren, gesteuerten und ungesteuerten dreidimensionalen Abloesungen
1978
52 Seiten, 42 Bilder, 79 Quellen
Aufsatz (Konferenz)
Englisch
Controlled and uncontrolled flow separation in three dimensions
TIBKAT | 1976
|Three-Dimensional Separations in Axial Compressors
Online Contents | 2005
|Interaction of Tip Clearance Flow and Three-Dimensional Separations in Axial Compressors
Online Contents | 2007
|Controlled and Uncontrolled Airspaces, VFR Routes, Terrain-II
British Library Conference Proceedings | 1988
|