Theoretical basis of the PANDA computer program for preliminary design of stiffened panels under combined in-plane loads

DOI10.1016/0045-7949(87)90280-XzbMath0619.73101MaRDI QIDQ3757507

David H. Bushnell

Publication date: 1987

Published in: Computers & Structures (Search for Journal in Brave)

zbMATH Keywords

ringrollingbifurcation bucklingelastic-plasticcylindricalisotropicflatminimum-weight designlocal instabilityelastic compositeminimum potential energygeneral instabilitypanel instabilitycombined in-plane loadscripplingfully populated 6\(\times 6\) thickness-integrated constitutive matricesPANDAPANDA 2stringer-stiffened panels

Mathematics Subject Classification ID

Bifurcation and buckling (74G60) Optimization problems in solid mechanics (74P99) Software, source code, etc. for problems pertaining to mechanics of deformable solids (74-04)

Related Items (2)

Stability of smooth and ribbed shells of revolution in a nonuniform stress-strain state. (Survey) ⋮ Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regime

Uses Software

• PANDA
• BOSOR5

This page was built for publication: Theoretical basis of the PANDA computer program for preliminary design of stiffened panels under combined in-plane loads