Efficient uncertainty quantification applied to the aeroelastic analysis of a transonic wing

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Hosder, Serhat ^a,c   Walters, Robert W ^b   Balch, Michael ^b  

^a Architectural and Environmental Engineering   (United States)

^b VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^c Aerospace and Ocean Engineering Department   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; ANGLE OF ATTACK; CURVE FITTING; DAMPING; FLUTTER (AERODYNAMICS); INTELLIGENT SYSTEMS; MACH NUMBER; MONTE CARLO METHODS; POLYNOMIAL APPROXIMATION; SENSITIVITY ANALYSIS; STOCHASTIC SYSTEMS; TRANSIENT ANALYSIS; WINGS;

AEROELASTIC ANALYSIS; COMPUTATIONAL COSTS; FREE STREAM MACH NUMBERS; POLYNOMIAL CHAOS EXPANSION; RESPONSE SURFACE APPROXIMATION; TRANSIENT AEROELASTIC RESPONSE; UNCERTAIN PARAMETERS; UNCERTAINTY QUANTIFICATIONS;

UNCERTAINTY ANALYSIS;

EID: 78149487064     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-729     Document Type: Conference Paper

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