보강된 복합적층 원통형패널의 좌굴거동
Buckling behavior of stiffened laminated composite cylindrical panel was studied using linear and nonlinear deformation theory. Various buckling load factors are obatined for stiffened laminated composite cylindrical panels with rectangular type longitudinal stiffeners and various longitudinal lengt...
Gespeichert in:
| Veröffentlicht in: | 한국생산제조학회지 2003, 12(5), , pp.88-93 |
|---|---|
| Hauptverfasser: | , , , |
| Format: | Artikel |
| Sprache: | kor |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| Zusammenfassung: | Buckling behavior of stiffened laminated composite cylindrical panel was studied using linear and nonlinear deformation theory. Various buckling load factors are obatined for stiffened laminated composite cylindrical panels with rectangular type longitudinal stiffeners and various longitudinal length to radius ratio, which made from Carbon/Epoxy USN150 prepreg and are simply-supported on four edges under uniaxial compression. Buckling behavior design analyses are carried out by the nonlinear search optimizer, ADS. KCI Citation Count: 0 |
|---|---|
| ISSN: | 2508-5093 2508-5107 |