Aeroelastic tailoring of high-aspect-ratio composite joined-wing UAV
For the high-aspect-ratio composite joined-wing UAV, as the geometric nonlinear significant effect, nonlinear aeroelastic analysis method should be applied when study its aeroelastic tailoring method. In the paper, based on the secondary development of MSC/Nastran software with Direct matrix abstrac...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
JVE International
2017-06-01
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| Series: | Mathematical Models in Engineering |
| Subjects: | |
| Online Access: | https://www.jvejournals.com/article/18505 |