作者: A. CUTLER , P. BRADSHAW
DOI: 10.2514/6.1986-1071
关键词: Delta wing 、 Vortex 、 Flow visualization 、 Aerospace engineering 、 Boundary layer 、 Wake 、 Wing 、 Turbulence 、 Mechanics 、 Flow separation 、 Physics
摘要: This paper presents the preliminary results of a long-term investigation interaction strong longitudinal vortices with turbulent boundary layers. A pair trailing is generated by delta wing, which mounted ahead flat plate so that merge layer on upper surface plate, while non-rolled-up part delta-wing wake passes below plate. approximates an aircraft wing close-coupled canard. The measurements show how boundary-layer fluid first subjected to large cross flow and then transported away from circulate around vortex core.