Validation of UAV wing structural model for finite element analysis
Finite element method is increasingly used in the analysis of aircraft structures, including Unmanned Aerial Vehicles (UAVs). The structural model used for finite element analysis however needs to be validated in order to ensure that it correctly represents the physical behaviour of the actual struc...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Published: |
Penerbit UTM Press
2014
|
| Subjects: |