A surrogate model approach in 2D versus 3D flapping wing aerodynamic analysis

12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, MAO

Volumn , Issue , 2008, Pages

  Trizila, Pat ^a   Kang, Chang Kwon ^a   Visbal, Miguel ^b   Shyy, Wei ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; KINEMATICS; LIFT; SENSITIVITY ANALYSIS; VORTEX FLOW;

ANGULAR AMPLITUDE; DESIGN VARIABLES; GLOBAL SENSITIVITY ANALYSIS; KINEMATIC PARAMETERS; LEADING-EDGE VORTICES; NON-LINEAR RESPONSE; OFF-DESIGN POINTS; POWER REQUIREMENT;

WINGS;

EID: 78049504896     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-5914     Document Type: Conference Paper

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