A new approach of creating a finite element stick model for flutter analysis
The article describes a new approach of creating a finite element stick model for the purpose of the aircraft flutter analysis. The control surface properties are merged with a lifting surface element as a special degree of freedom (DOF). The number of DOF for the coordination system is increased fr...
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| Format: | Article |
| Language: | English |
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EDP Sciences
2019-01-01
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| Series: | MATEC Web of Conferences |
| Online Access: | https://www.matec-conferences.org/articles/matecconf/pdf/2019/53/matecconf_easn2019_01015.pdf |