Simultaneous cost and weight minimization of postbuckled composite panels under combined compression and shear

Structural and Multidisciplinary Optimization

Volumn 21, Issue 5, 2001, Pages 372-382

  Kassapoglou, C ^a   Dobyns, A L ^a  

^a SIKORSKY AIRCRAFT CORPORATION   (United States)

Author keywords

Cost and weight minimization; Optimization; Pareto set; Post buckled composite panels

Indexed keywords

BUCKLING; COMPOSITE MATERIALS; COSTS; OPTIMIZATION; RESIN TRANSFER MOLDING;

POST-BUCKLED COMPOSITE PANELS;

STRUCTURAL PANELS;

EID: 0035396980     PISSN: 1615147X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s001580100116     Document Type: Article

References (15)

1. Über algorithmen zur ermittlung und charaketerisierung pareto-optimaler lösungen bei entwurfsaufgaben elastischer tragwerke
2. Advanced technology composite fuselage
3. Simultaneous cost and weight minimization of composite-stiffened panels under compression and shear
4. Minimum cost and weight design of fuselage frames, Part A: Design constraints and manufacturing process characteristics
5. Minimum cost and weight design of fuselage frames, Part B: Cost considerations, optimization, and results
6. The use of COSTADE in developing composite commercial aircraft fuselage structures
7. Robotics key to curbing Premier 1 production costs
8. Structural optimization by methods of feasible directions
9. Multicriterion design of fuzzy structural systems using immune network simulation