Wing Structure Static Analysis using Superelement
This paper describes the use of superelement for the stress and deflection analysis of a typical fighter wing structure. Three methods of analyses were carried out and compared: practical/theoretical analysis; finite element analysis with the conventional element modeling approach; and finite elemen...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Online Access: | View Fulltext in Publisher |