Robust structural optimization of plate wing corresponding to bifurcation in higher mode flutter

Structural and Multidisciplinary Optimization

Volumn 30, Issue 6, 2005, Pages 437-446

  Odaka, Y ^a   Furuya, H ^a  

^a TOKYO INSTITUTE OF TECHNOLOGY   (Japan)

Author keywords

Aeroelasticity; Analysis; Jump; Sensitivity; Supersonic flutter; Uncertainty

Indexed keywords

ANALYSIS; CONVERGENCE OF NUMERICAL METHODS; FLUTTER (AERODYNAMICS); PRESSURE EFFECTS; ROBUSTNESS (CONTROL SYSTEMS); STRUCTURAL ANALYSIS; STRUCTURAL DESIGN; WINGS;

AEROELASTICITY; JUMP; SENSITIVITY; SUPERSONIC FLUTTER; UNCERTAINTY;

OPTIMIZATION;

EID: 28344449812     PISSN: 1615147X     EISSN: 16151488     Source Type: Journal    
DOI: 10.1007/s00158-005-0538-9     Document Type: Article

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