Addendum to a theoretical and experimental study of the boundary layer flow on a 45 degrees swept back wing

Walton, J.2013-06-262013-06-261957-11http://dspace.lib.cranfield.ac.uk/handle/1826/7978COA report 109 describes Flight Tests carried out on a swept back half wing of double elliptical section to investigate the nature of the boundary layer flow, with particular reference to Bounday Layer Instability and subsequent transition.enAddendum to a theoretical and experimental study of the boundary layer flow on a 45 degrees swept back wingReport