Load case selection technique for combined modal finite element approach of high aspect ratio wing models
A high aspect ratio wing is known to exhibit high deflection even at relatively low aerodynamic loading, making it susceptible to geometric nonlinearity. However, integrating linear and nonlinear static solutions through conventional finite element demands significant time and effort. Therefore, res...
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| Main Authors: | , , , , |
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| Format: | Article |
| Published: |
National Cheng Kung University
2023
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| Online Access: | http://psasir.upm.edu.my/id/eprint/110079/ https://www.airitilibrary.com/Article/Detail/P20140627004-N202308290008-00003 |
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