Experimental study of UTM-LST generic half model transport aircraft
This paper presents the experimental results from the investigation carried out at the UTM Low Speed wind tunnel facility (UTM-LST) on a half model generic transport aircraft at several configurations of primary control surfaces (flap, aileron and elevator). The objective is to measure the aerodynam...
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| Main Authors: | , , , |
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| Format: | Conference or Workshop Item |
| Published: |
Institute of Physics Publishing
2016
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| Subjects: | |
| Online Access: | http://eprints.utm.my/72973/ http://eprints.utm.my/72973/ |
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