Searching for just a few words should be enough to get started. If you need to make more complex queries, use the tips below to guide you.
Article type: Research Article
Authors: Bose, N.
Affiliations: Department of Naval Architecture and Ocean Engineering, University of Glasgow, U.K.
Abstract: A strip theory approach is described which is designed to obtain the lift and drag coefficients of a wind turbine rotor operating as an autogyro. This theory is an extension of the autogyro theory which was developed during the 1920’s and 1930’s. The theory has been extended to include the effects of varying blade planform, blade section and blade twist. This was necessary in order to evaluate the performance of the variable pitch rotors used for the propulsion of marine craft when operating in beam winds in the autogyro mode. Rotors with flapping blades were not considered. A computer program has been written incorporating this method. Results have been obtained for two example autogyro rotors using this program and these are presented here to give an idea of the typical performance of a wind turbine rotor when operating in the autogyro mode. The characteristics of autogyros are discussed in relation to their use as propulsion systems for wind propelled marine vehicles.
DOI: 10.3233/ISP-1983-3034802
Journal: International Shipbuilding Progress, vol. 30, no. 348, pp. 179-186, 1983
IOS Press, Inc.
6751 Tepper Drive
Clifton, VA 20124
USA
Tel: +1 703 830 6300
Fax: +1 703 830 2300
[email protected]
For editorial issues, like the status of your submitted paper or proposals, write to [email protected]
IOS Press
Nieuwe Hemweg 6B
1013 BG Amsterdam
The Netherlands
Tel: +31 20 688 3355
Fax: +31 20 687 0091
[email protected]
For editorial issues, permissions, book requests, submissions and proceedings, contact the Amsterdam office [email protected]
Inspirees International (China Office)
Ciyunsi Beili 207(CapitaLand), Bld 1, 7-901
100025, Beijing
China
Free service line: 400 661 8717
Fax: +86 10 8446 7947
[email protected]
For editorial issues, like the status of your submitted paper or proposals, write to [email protected]
如果您在出版方面需要帮助或有任何建, 件至: [email protected]