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

Simple item page
dc.contributor.authorWalton, J.
dc.date.accessioned2013-06-26T10:52:34Z
dc.date.available2013-06-26T10:52:34Z
dc.date.issued1957-11
dc.description.abstractCOA 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.sponsorshipM.O.S. contract No. 6/ Aircraft/14002/C.B.6 (a)en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7978
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reporten_UK
dc.relation.ispartofseries109 Addendumen_UK
dc.titleAddendum to a theoretical and experimental study of the boundary layer flow on a 45 degrees swept back wingen_UK
dc.typeReporten_UK

Files

Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
COA_Report_No_109Add _Nov_1957.pdf
Size:
3.19 MB
Format:
Adobe Portable Document Format
Download
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.79 KB
Format:
Item-specific license agreed upon to submission
Description:
Download

Collections

CoA. Reports