Concise orthogonal representation of supercritical airfoils
Concise orthogonal representation of supercritical airfoils
The combination of optimization algorithms and computational fluid dynamics offers promise for the development of improved aerodynamic designs. Optimization strategies have a common requirement for representation of geometry by a number of design parameters. For wing design the parameterization is generally separable into a representation of the planform and the representation of airfoil sections at a number of spanwise positions. The representation of airfoil sections is considered here with particular emphasis on the requirements of conceptual wing design.
580-582
Robinson, G.M.
e32dc9d8-2d9d-433d-818e-9daaf090b2c2
Keane, A.J.
26d7fa33-5415-4910-89d8-fb3620413def
2001
Robinson, G.M.
e32dc9d8-2d9d-433d-818e-9daaf090b2c2
Keane, A.J.
26d7fa33-5415-4910-89d8-fb3620413def
Robinson, G.M. and Keane, A.J.
(2001)
Concise orthogonal representation of supercritical airfoils.
Journal of Aircraft, 38 (3), .
Abstract
The combination of optimization algorithms and computational fluid dynamics offers promise for the development of improved aerodynamic designs. Optimization strategies have a common requirement for representation of geometry by a number of design parameters. For wing design the parameterization is generally separable into a representation of the planform and the representation of airfoil sections at a number of spanwise positions. The representation of airfoil sections is considered here with particular emphasis on the requirements of conceptual wing design.
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robi_01.pdf
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Published date: 2001
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Local EPrints ID: 21850
URI: http://eprints.soton.ac.uk/id/eprint/21850
ISSN: 0021-8669
PURE UUID: 834221a6-f942-4945-af5b-a1b862c61def
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Date deposited: 16 Mar 2006
Last modified: 16 Mar 2024 02:53
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G.M. Robinson
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