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Full-Field Deformation Measurement of Morphing Wings

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Mechanics of Composite and Multi-functional Materials, Volume 5
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Abstract

A micro air vehicle that can achieve a versatile flight condition is being designed. One way of achieving such versatility is through biomimicry. One aspect of this design utilizes a bird-like wing that changes shape to match four flight regimes; take-off-and -landing, cruise, high speed dash and one that enhances maneuverability. A joint mechanism using a tendon actuator between the inboard and the outboard portions of the wing is used to modify wing sweep. Macro fiber composites (MFCs) piezoelectric actuators in a bi-morph configuration are incorporated into the MAVs as control mechanism. Camber changes are implemented with tendon actuators. Finite element is used to model the wing section and perform a full-field deformation study and compared with experimental results. Digital image correlation is used to validate the wing deformations predicted by finite element method (FEA).

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References

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Acknowledgements

The authors would like to thank the STTR program under the Air Force Office of Scientific Research for the funding.

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Correspondence to M. M. Mennu .

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© 2020 Society for Experimental Mechanics, Inc.

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Mennu, M.M., Tran, B., Ifju, P.G., Santamaria, E. (2020). Full-Field Deformation Measurement of Morphing Wings. In: Singh, R., Slipher, G. (eds) Mechanics of Composite and Multi-functional Materials, Volume 5. Conference Proceedings of the Society for Experimental Mechanics Series. Springer, Cham. https://doi.org/10.1007/978-3-030-30028-9_16

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  • DOI: https://doi.org/10.1007/978-3-030-30028-9_16

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-030-30027-2

  • Online ISBN: 978-3-030-30028-9

  • eBook Packages: EngineeringEngineering (R0)

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