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

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

Walton, J.
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/4783

Description:

 
COA 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.
 
M.O.S. contract No. 6/ Aircraft/14002/C.B.6 (a)
 

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