Drag reduction in aircraft model using elliptical winglet
Aerodynamic characteristics for the aircraft model with NACA (National Advisory Committee for Aeronautics) wing No. 65-3-218 have been studied using subsonic wind tunnel of 1000 mm x 1000 mm rectangular test section and 2500 mm long of Aerodynamics Laboratory Faculty of Engineering (Universiti Putra...
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| Format: | Journal |
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IEM Journal, The Institution of Engineers Malaysia
2005
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| Online Access: | http://www.myjurnal.my/public/article-view.php?id=67008 |