Robust airfoil design with respect to boundary layer transition

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn , Issue , 2009, Pages

  Zhao, Liangyu ^a   Dawes, W N ^b   Parks, Geoffrey ^b   Jarrett, Jerome P ^b   Yang, Shuxing ^a  

^a BEIJING INSTITUTE OF TECHNOLOGY   (China)

^b UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; AVIATION; CAMBERS; DESIGN AIDS; LIFT; LOCATION; MONTE CARLO METHODS; STATISTICS; STOCHASTIC SYSTEMS; STRUCTURAL DYNAMICS;

AIRFOIL DESIGN; BOUNDARY LAYER TRANSITIONS; DETERMINISTIC DESIGN; MAXIMUM LIFT COEFFICIENT; MAXIMUM THICKNESS; POLYNOMIAL CHAOS; STANDARD DEVIATION; STOCHASTIC VARIABLE;

BOUNDARY LAYERS;

EID: 84855638792     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-2273     Document Type: Conference Paper

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