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/id/eprint/72973/ https://www.scopus.com/inward/record.uri?eid=2-s2.0-84998774621&doi=10.1088%2f1757-899X%2f152%2f1%2f012007&partnerID=40&md5=26ad21ba7c66225e5e34cfd3fb2f0e09 |
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