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).

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Description/Abstract

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 (Project Report)
Additional Information: ISSN 0140-3818
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics
V Naval Science > VM Naval architecture. Shipbuilding. Marine engineering
ePrint ID: 43551
Date :
Date Event
1985Published
Date Deposited: 24 Jan 2007
Last Modified: 16 Apr 2017 18:48
Further Information:Google Scholar
URI: http://eprints.soton.ac.uk/id/eprint/43551

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