A novel sensitivity analysis method for high fidelity multidisciplinary optimization of aero-structural systems

38th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2000, Pages

  Giunta, Anthony A ^a,b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b SANDIA NATIONAL LABORATORIES   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; AIRCRAFT MODELS; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; FINITE DIFFERENCE METHOD; MODAL ANALYSIS; NASA; SENSITIVITY ANALYSIS; STRUCTURAL OPTIMIZATION; SUPERSONIC AIRCRAFT; WINGS;

AEROELASTIC AIRCRAFT MODELS; COMPUTATIONALLY EFFICIENT; CONCURRENT COMPUTATION; FINITE DIFFERENCE APPROACH; FINITE ELEMENT ANALYSIS SOFTWARE; GLOBAL SENSITIVITY EQUATION; MULTI-DISCIPLINARY OPTIMIZATIONS; STRUCTURAL ANALYSIS SOFTWARES;

STRUCTURAL ANALYSIS;

EID: 85088756410     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-683     Document Type: Conference Paper

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