Concise orthogonal representation of supercritical airfoils

Journal of Aircraft

Volumn 38, Issue 3, 2001, Pages 580-583

  Robinson, G M ^a   Keane, A J ^b,c  

^a DEFENCE SCIENCE AND TECHNOLOGY LABORATORY   (United Kingdom)

^b UNIVERSITY OF SOUTHAMPTON   (United Kingdom)

^c School of Engineering Sciences   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; CURVE FITTING; DESIGN; DRAG; FUNCTIONS; ITERATIVE METHODS; LEAST SQUARES APPROXIMATIONS; LIFT; OPTIMIZATION; REYNOLDS NUMBER; TRANSPORT AIRCRAFT; WINGS;

GEOMETRICALLY ORTHOGONAL BASE FUNCTIONS; MACH NUMBER; SUPERCRITICAL AIRFOILS; WING DESIGN;

AIRFOILS;

EID: 0035333964     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2803     Document Type: Article

References (13)

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7. Airfoil design and optimization by the one-shot method
8. Geometric analysis of wing sections
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10. VGK method for two-dimensional airfoil sections
11. NASA supercritical airfoils-a matrix of family-related airfoils
12. A case for multi-level optimization in aeronautical design