Abstract
The critical buckling loads of unsymmetrically laminated rectangular plates with a given material system and subjected to combined lateral and inplane loads are maximized with respect to fiber orientations by using a sequential linear programming method together with a simple move-limit strategy. Significant influence of plate aspect ratios, central circular cutouts, lateral loads and end conditions on the optimal fiber orientations and the associated optimal buckling loads of unsymmetrically laminated plates has been shown through this investigation.
| Original language | English |
|---|---|
| Pages (from-to) | 19-33 |
| Number of pages | 15 |
| Journal | Structural Engineering and Mechanics |
| Volume | 7 |
| Issue number | 1 |
| DOIs | |
| Publication status | Published - 1999 Jan 1 |
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All Science Journal Classification (ASJC) codes
- Civil and Structural Engineering
- Building and Construction
- Mechanics of Materials
- Mechanical Engineering
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Buckling optimization of unsymmetrically laminated plates under transverse loads. / Hu, Hsuan Teh.
In: Structural Engineering and Mechanics, Vol. 7, No. 1, 01.01.1999, p. 19-33.Research output: Contribution to journal › Article
TY - JOUR
T1 - Buckling optimization of unsymmetrically laminated plates under transverse loads
AU - Hu, Hsuan Teh
PY - 1999/1/1
Y1 - 1999/1/1
N2 - The critical buckling loads of unsymmetrically laminated rectangular plates with a given material system and subjected to combined lateral and inplane loads are maximized with respect to fiber orientations by using a sequential linear programming method together with a simple move-limit strategy. Significant influence of plate aspect ratios, central circular cutouts, lateral loads and end conditions on the optimal fiber orientations and the associated optimal buckling loads of unsymmetrically laminated plates has been shown through this investigation.
AB - The critical buckling loads of unsymmetrically laminated rectangular plates with a given material system and subjected to combined lateral and inplane loads are maximized with respect to fiber orientations by using a sequential linear programming method together with a simple move-limit strategy. Significant influence of plate aspect ratios, central circular cutouts, lateral loads and end conditions on the optimal fiber orientations and the associated optimal buckling loads of unsymmetrically laminated plates has been shown through this investigation.
UR - http://www.scopus.com/inward/record.url?scp=0032715292&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0032715292&partnerID=8YFLogxK
U2 - 10.12989/sem.1999.7.1.019
DO - 10.12989/sem.1999.7.1.019
M3 - Article
AN - SCOPUS:0032715292
VL - 7
SP - 19
EP - 33
JO - Structural Engineering and Mechanics
JF - Structural Engineering and Mechanics
SN - 1225-4568
IS - 1
ER -