Contact-aided compliant mechanisms for morphing aircraft skin

Research output: Chapter in Book/Report/Conference proceedingConference contribution

15 Citations (Scopus)

Abstract

Sandwich structures consisting of contact-aided compliant mechanisms are presented for morphing aircraft skin. A contact mechanism is used to alleviate stresses and to decrease the oul-of-plane deflection. A methodology to design such mechanisms, which takes into account the aerodynamic loads, is presented. The method is applied to a small UAV and results are compared with those of honeycomb structures in terms of structural mass, global strain and maximum stresses. Different material models such as linearly elastic and multi-linear elastic are considered. For linearly elastic materials, contact-induced stress-relief is advantageous and for nonlinear elastic materials, reduction of transverse deflection due to contact is useful. In either ease, the structural mass of the contact-aided structures is less than that of the corresponding non-contact structures.

Original languageEnglish (US)
Title of host publicationModeling, Signal Processing, and Control for Smart Structures 2008
Volume6926
DOIs
StatePublished - Jun 2 2008
EventModeling, Signal Processing, and Control for Smart Structures 2008 - San Diego, CA, United States
Duration: Mar 10 2008Mar 12 2008

Other

OtherModeling, Signal Processing, and Control for Smart Structures 2008
CountryUnited States
CitySan Diego, CA
Period3/10/083/12/08

Fingerprint

Compliant mechanisms
Compliant Mechanism
Morphing
Skin
aircraft
Aircraft
Contact
deflection
aerodynamic loads
Honeycomb structures
Elastic Material
honeycomb structures
Aerodynamic loads
Stress relief
Sandwich structures
sandwich structures
Deflection
Unmanned aerial vehicles (UAV)
Linearly
Sandwich Structures

All Science Journal Classification (ASJC) codes

  • Electronic, Optical and Magnetic Materials
  • Condensed Matter Physics
  • Computer Science Applications
  • Applied Mathematics
  • Electrical and Electronic Engineering

Cite this

Mehta, V., Frecker, M. I., & Lesieutre, G. A. (2008). Contact-aided compliant mechanisms for morphing aircraft skin. In Modeling, Signal Processing, and Control for Smart Structures 2008 (Vol. 6926). [69260C] https://doi.org/10.1117/12.773599
Mehta, Vipul ; Frecker, Mary I. ; Lesieutre, George A. / Contact-aided compliant mechanisms for morphing aircraft skin. Modeling, Signal Processing, and Control for Smart Structures 2008. Vol. 6926 2008.
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Mehta, V, Frecker, MI & Lesieutre, GA 2008, Contact-aided compliant mechanisms for morphing aircraft skin. in Modeling, Signal Processing, and Control for Smart Structures 2008. vol. 6926, 69260C, Modeling, Signal Processing, and Control for Smart Structures 2008, San Diego, CA, United States, 3/10/08. https://doi.org/10.1117/12.773599

Contact-aided compliant mechanisms for morphing aircraft skin. / Mehta, Vipul; Frecker, Mary I.; Lesieutre, George A.

Modeling, Signal Processing, and Control for Smart Structures 2008. Vol. 6926 2008. 69260C.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Mehta V, Frecker MI, Lesieutre GA. Contact-aided compliant mechanisms for morphing aircraft skin. In Modeling, Signal Processing, and Control for Smart Structures 2008. Vol. 6926. 2008. 69260C https://doi.org/10.1117/12.773599