Addendum to a theoretical and experimental study of the boundary layer flow on a 45 degrees swept back wing
Date
1957-11
Authors
Supervisor/s
Journal Title
Journal ISSN
Volume Title
Publisher
College of Aeronautics, Cranfield
Department
Type
Report
ISSN
Format
Free to read from
Citation
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.
Description
Software Description
Software Language
Github
Keywords
DOI
Rights
Relationships
Relationships
Supplements
Funder/s
M.O.S. contract No. 6/ Aircraft/14002/C.B.6 (a)