Multidisciplinary design optimization of a built-up wing structure with a tip missile

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 3, Issue , 2002, Pages 1739-1748

  Jun, Seungmoon ^a   Tischler, V A ^a   Venkayya, V B ^a  

^a Agency for Defence Development   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AUTOMATION; FINITE ELEMENT METHOD; FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS; MISSILES; STIFFNESS; STRUCTURAL DESIGN; STRUCTURAL OPTIMIZATION;

MULTIDISCIPLINARY OPTIMIZATION;

WINGS;

EID: 0036076057     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

1. Effect of store aerodynamics on wing/store flutter
2. Optimization of Wing Tip Store Modeling
3. Wind tunnel correlation study of aerodynamic modeling for f/a-18 wing-store tip-missile flutter
4. Transonic aeroelasticity of wing with tip stores
5. Evaluation of computational aeroelasticity codes for loads and flutter
6. Structural optimization using computational aerodynamics
7. Automated structural optimization system (ASTROS)
8. Automated structural optimization system (ASTROS)
9. Aeroelastic tailoring of composite structures
10. Influence of structural and aerodynamic modeling on flutter analysis
11. Development of the aerodynamic/aeroservoelastic modules in ASTROS
12. Development of the Aerodynamic/Aeroservoelastic Modules in ASTROS
13. An efficient feasible directions algorithm for design synthesis
14. Approximation concepts for efficient structural synthesis