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Nonlinear aeroelastic analysis with inextensible plate theory including correlation with experiment

Publication ,  Journal Article
Tang, D; Gibbs, SC; Dowell, EH
Published in: AIAA Journal
January 1, 2015

A computational aeroelastic model is presented for a cantilevered plate rotated from a position with the clamped edge normal to the flow (0 deg) to where the clamped edge is aligned with the flow (90 deg) using a new inextensible plate theory. A large-amplitude limit-cycle oscillation has been observed beyond the linear flutter speed in both the computations and in a wind-tunnel experiment. The computations and experiments for the limit-cycle oscillation response of the several yawed plate aeroelastic models show that the inextensible plate theory produces results in good agreement with the measurements. Also, a comparison with results obtained using von Kármán's nonlinear plate theory has been made.

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Published In

AIAA Journal

DOI

ISSN

0001-1452

Publication Date

January 1, 2015

Volume

53

Issue

5

Start / End Page

1299 / 1308

Related Subject Headings

  • Aerospace & Aeronautics
  • 4012 Fluid mechanics and thermal engineering
  • 4001 Aerospace engineering
  • 0913 Mechanical Engineering
  • 0905 Civil Engineering
  • 0901 Aerospace Engineering
 

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Tang, D., Gibbs, S. C., & Dowell, E. H. (2015). Nonlinear aeroelastic analysis with inextensible plate theory including correlation with experiment. AIAA Journal, 53(5), 1299–1308. https://doi.org/10.2514/1.J053385
Tang, D., S. C. Gibbs, and E. H. Dowell. “Nonlinear aeroelastic analysis with inextensible plate theory including correlation with experiment.” AIAA Journal 53, no. 5 (January 1, 2015): 1299–1308. https://doi.org/10.2514/1.J053385.
Tang D, Gibbs SC, Dowell EH. Nonlinear aeroelastic analysis with inextensible plate theory including correlation with experiment. AIAA Journal. 2015 Jan 1;53(5):1299–308.
Tang, D., et al. “Nonlinear aeroelastic analysis with inextensible plate theory including correlation with experiment.” AIAA Journal, vol. 53, no. 5, Jan. 2015, pp. 1299–308. Scopus, doi:10.2514/1.J053385.
Tang D, Gibbs SC, Dowell EH. Nonlinear aeroelastic analysis with inextensible plate theory including correlation with experiment. AIAA Journal. 2015 Jan 1;53(5):1299–1308.
Journal cover image

Published In

AIAA Journal

DOI

ISSN

0001-1452

Publication Date

January 1, 2015

Volume

53

Issue

5

Start / End Page

1299 / 1308

Related Subject Headings

  • Aerospace & Aeronautics
  • 4012 Fluid mechanics and thermal engineering
  • 4001 Aerospace engineering
  • 0913 Mechanical Engineering
  • 0905 Civil Engineering
  • 0901 Aerospace Engineering