Aeroelastic tailoring of a plate wing with functionally graded materials

Peter D. Dunning, Bret K. Stanford, H. Alicia Kim, Christine V. Jutte

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

Abstract

This work explores the use of functionally graded materials for the aeroelastic tailoring of a metallic cantilevered plate-like wing. Pareto trade-off curves between dynamic stability (flutter) and static aeroelastic stresses are obtained for a variety of grading strategies. A key comparison is between the effectiveness of material grading, geometric grading (i.e., plate thickness variations), and using both simultaneously. The introduction of material grading does, in some cases, improve the aeroelastic performance. This improvement, and the physical mechanism upon which it is based, depends on numerous factors: the two sets of metallic material parameters used for grading, the sweep of the plate, the aspect ratio of the plate, and whether the material is graded continuously or discretely.

Original languageEnglish
Title of host publication55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference
PublisherSciTech
ISBN (Electronic)978-1-62410-314-8
DOIs
Publication statusPublished - 2014
Event55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference - SciTech Forum and Exposition 2014 - National Harbor, MD, United States
Duration: 13 Jan 201417 Jan 2014

Conference

Conference55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference - SciTech Forum and Exposition 2014
CountryUnited States
CityNational Harbor, MD
Period13/01/1417/01/14

Fingerprint

Functionally graded materials
Aspect ratio

ASJC Scopus subject areas

  • Civil and Structural Engineering
  • Mechanics of Materials
  • Building and Construction
  • Architecture

Cite this

Dunning, P. D., Stanford, B. K., Alicia Kim, H., & Jutte, C. V. (2014). Aeroelastic tailoring of a plate wing with functionally graded materials. In 55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference SciTech. https://doi.org/10.2514/6.2014-0344

Aeroelastic tailoring of a plate wing with functionally graded materials. / Dunning, Peter D.; Stanford, Bret K.; Alicia Kim, H.; Jutte, Christine V.

55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference. SciTech, 2014.

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

Dunning, PD, Stanford, BK, Alicia Kim, H & Jutte, CV 2014, Aeroelastic tailoring of a plate wing with functionally graded materials. in 55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference. SciTech, 55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference - SciTech Forum and Exposition 2014, National Harbor, MD, United States, 13/01/14. https://doi.org/10.2514/6.2014-0344
Dunning PD, Stanford BK, Alicia Kim H, Jutte CV. Aeroelastic tailoring of a plate wing with functionally graded materials. In 55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference. SciTech. 2014 https://doi.org/10.2514/6.2014-0344
Dunning, Peter D. ; Stanford, Bret K. ; Alicia Kim, H. ; Jutte, Christine V. / Aeroelastic tailoring of a plate wing with functionally graded materials. 55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference. SciTech, 2014.
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