Evolutionary structural optimization of plate wing for supersonic flutter

19th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2001, Pages

  Furuya, Hiroshi ^a,b   Fukuchi, Isao ^a,b  

^a TOKYO INSTITUTE OF TECHNOLOGY   (Japan)

^b Department of Built Environment ^*  (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

DELTA WING AIRCRAFT; FLUTTER (AERODYNAMICS); PLATES (STRUCTURAL COMPONENTS); SHAPE OPTIMIZATION;

BENDING STIFFNESS; EQUIVALENT THICKNESS; EVOLUTIONARY STRUCTURAL OPTIMIZATION; OBJECTIVE FUNCTIONS; OPTIMIZATION PROBLEMS; OPTIMIZATION PROCEDURES; PERFORMANCE AND RELIABILITIES; SUPERSONIC FLUTTER;

STRUCTURAL OPTIMIZATION;

EID: 85067319149     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1631     Document Type: Conference Paper

References (5)

1. Vanderplaats, G.N., Structural Design Optimization Status and Direction, AIAA Paper 97-1407, 38th AIAAIASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Kissimmee, FL, Apr. 1997.
2. Vitali, R., Park, O., Haftka, Raphael T., and Sankar, Bhavani V., Structural Optimization of a Hat Stiffened Panel by Response Surface Techniques, AIAA Paper 97-1151, 38th AIAAIASMEI-ASCEIAHSIASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Kissimmee, FL, Apr. 1997.
3. Sobieski, I.P. and Kroo, I.M., Collaborative Optimization Using Response Surface Estimation, AIAA Paper 98-0915, 36th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, Jan. 1998.
4. Battoo, Rupinder S. and de Visser, J.A.P., Aeroe-lastic and Strength Optimization of a Large Aircraft Wing with Wing Parameter Variations, AIAA Paper 98-1821, 39th AIAAIASMEIASCEI-AHSIASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Long Beach, CA, Apr. 1998.
5. Kim, Nam C, et al., Optimal Sizing and Placement of Piezo-Actuators for Active Flutter Suppression, Smart Materials & Structures, Vol.5, No.2, 1996, pp.216-224.