Composite wing structural design optimization with continuity constraints

19th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2001, Pages

  Liu, Boyang ^a   Haftka, Raphael T ^a  

^a University of Florida   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; INDIUM COMPOUNDS; PAPER LAMINATES; STRUCTURAL DESIGN; STRUCTURAL OPTIMIZATION; STRUCTURE (COMPOSITION); WINGS;

COMPLEX COMPOSITE STRUCTURES; COMPOSITE WING; CONTINUITY CONSTRAINTS; HIGH STIFFNESS; STRENGTH TO WEIGHT RATIO; STRUCTURAL DESIGN OPTIMIZATION;

LAMINATED COMPOSITES;

EID: 85055913153     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1205     Document Type: Conference Paper

References (4)

1. Liu, B., Haftka, R.T., and Akgun, M. A., Two-level Composite Wing Structural Optimization Using Response Surface, Structural and Multidisciplinary Optimization, 20, pp.87-96, 2000
2. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Material Conference, Kissimmee, FL, April 7-10, 1997, Part 2, pp. 1204-1214 AIAA Paper 97-1051.
3. Schmit, L.A., and Mehrinfar, M., Multilevel Optimum Design of Structures with Fiber-Composite Stiffened Panel Components, AIAA J., 20(1), 1982, pp. 138-147.
4. Vanderplaats, Miura and Associates, Inc., GENESIS User Manual, Version 6.0, Dec. 2000