Wind tunnel test on generic agusta-bell 206b helicopter tail rotor blades
A low speed wind tunnel test was conducted for a full-scaled generic model of Agusta-Bell 206B helicopter tail rotor blades in the Universiti Teknologi Malaysia-Low Speed Tunnel (UTM- LST). The purpose of this paper is to conduct the experimental research for gaining information on general aerodynam...
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| Format: | Article |
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International Society of Ocean, Mechanical and Aerospace Scientists and Engineers
2015
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