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On the Design of Morphing Airfoils using Spinal Structures

Record type: Conference or Workshop Item (Paper)

In this paper the design of spinal structures for the control of
morphing airfoils is examined. The aim is to find structures that,
when suitably loaded, can alter the aerodynamic shape of a
cladding that forms the airfoil. Morphing through different
cambered airfoils to achieve aerodynamic properties for different
maneuvers is then possible by exploiting a range of incremental
non-linear structural solutions. Further, by using structures that
are acting in the post-buckling regime, it is possible to obtain
significant changes in shape with only modest changes in applied
load. The structure also presents enhanced aeroelastic properties.
Results are formulated in terms of the aerodynamic properties of
the morphed airfoils using a shape optimized beam as the spinal
structure with fixed aerodynamic cladding.

Full text not available from this repository.

Citation

Ursache, Narcis M., Keane, A.J. and Bressloff, N.W. (1970) On the Design of Morphing Airfoils using Spinal Structures In Proceedings of the 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics. 10 pp, pp. 1-10. (doi:10.2514/6.2006-1796).

More information

Published date: 1 January 1970
Venue - Dates: 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2006-05-01 - 2006-05-04
Keywords: Morphing airfoils, structural optimization, inverse design, post-buckling, large displacements, beam-column, parameterization schemes, Discrete approach, NURBS parameterization

Identifiers

Local EPrints ID: 38000
URI: http://eprints.soton.ac.uk/id/eprint/38000
PURE UUID: e6755b9b-6bbf-4b79-bb54-926e46677307

Catalogue record

Date deposited: 30 May 2006
Last modified: 17 Jul 2017 15:40

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Contributors

Author: Narcis M. Ursache
Author: A.J. Keane
Author: N.W. Bressloff

University divisions

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