Load case selection guideline for combined modal finite element approach for static aeroelastic deformations of rectangular HAR wing models
High aspect ratio (HAR) and flexible wing models have multiple benefits. However, due to the nonlinear properties of this type of structure, the linear solution of static aeroelastic response is not sufficient to analyse the wing characteristics. Thus, making the option become more and more undes...
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| Format: | Thesis |
| Language: | English |
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2020
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| Online Access: | http://psasir.upm.edu.my/id/eprint/104252/1/THINESH%20AL%20CHANDRASEGARAN%20-%20%20IR.pdf |