Development of a two dimensional flow test section for a wind tunnel and its use with a hybrid flapped multiplane
Satchwell, C.J. (1985) Development of a two dimensional flow test section for a wind tunnel and its use with a hybrid flapped multiplane. Southampton, UK, University of Southampton, 24pp. (Ship Science Reports, 22).
- Version of Record
The report describes the development of a two dimensional flow wind tunnel test section, suitable for measuring lift. Its principal use was in developing aerofoils for windship propulsion and results for one of these provide an illustrative example. The results indicate that a C subscript L of around 4.2 can be achieved without flow separation and a C subscript LMAX of around 4.7 with separation.
|Item Type:||Monograph (Technical Report)|
|Additional Information:||ISSN 0140-3818|
|Subjects:||T Technology > TL Motor vehicles. Aeronautics. Astronautics
V Naval Science > VM Naval architecture. Shipbuilding. Marine engineering
|Divisions:||University Structure - Pre August 2011 > School of Engineering Sciences
|Date Deposited:||24 Jan 2007|
|Last Modified:||30 Sep 2015 08:36|
|RDF:||RDF+N-Triples, RDF+N3, RDF+XML, Browse.|
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