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

Walton, J.

dc.contributor.author	Walton, J.
dc.date.accessioned	2013-06-26T10:52:34Z
dc.date.available	2013-06-26T10:52:34Z
dc.date.issued	1957-11
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/7978
dc.description.abstract	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.	en_UK
dc.description.sponsorship	M.O.S. contract No. 6/ Aircraft/14002/C.B.6 (a)	en_UK
dc.language.iso	en	en_UK
dc.publisher	College of Aeronautics, Cranfield	en_UK
dc.relation.ispartofseries	College Report	en_UK
dc.relation.ispartofseries	109 Addendum	en_UK
dc.title	Addendum to a theoretical and experimental study of the boundary layer flow on a 45 degrees swept back wing	en_UK
dc.type	Report	en_UK