Bending-torsional flutter of a composite rectangular cantilever wing subjected to engine thrust

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

Abstract

The bending-torsional flutter characteristics of a cantilever composite wing subjected to engine thrust are presented. The engine thrust modeled as a follower force and the wing modeled as a two degree of freedom beam. In order to consider the spanwise and chordwise location and the properties of the engine location, the generalized function theory is used. Unsteady Theodorsen aerodynamic theory in time domain, is used. The general laminate composite theory is used for modeling the effects of the ply angles on the flutter boundary. The Ritz method is subsequently applied to convert the partial differential equations into a set of ordinary differential equations. In order to precisely consider the location of the engine Dirac delta function is used. Moreover, the numerical results are compared with the published results and excellent agreement is observed. Numerical results highlighting the effect of engine thrust on the wing instability, is presented.

Original languageEnglish
Title of host publicationAdvanced Materials Research II
Pages1568-1572
Number of pages5
DOIs
Publication statusPublished - 27 Feb 2012
Externally publishedYes
Event2nd International Conference on Advanced Material Research - Chengdu, China
Duration: 7 Jan 20128 Jan 2012
Conference number: 2
http://www.icamr.org/2012.html

Publication series

NameAdvanced Materials Research
Volume463-464
ISSN (Print)1022-6680

Conference

Conference2nd International Conference on Advanced Material Research
Abbreviated titleICAMR 2012
CountryChina
CityChengdu
Period7/01/128/01/12
Internet address

Fingerprint

Flutter (aerodynamics)
Engines
Composite materials
Delta functions
Ordinary differential equations
Partial differential equations
Laminates
Aerodynamics

Cite this

Amoozgar, M. R., & Irani, S. (2012). Bending-torsional flutter of a composite rectangular cantilever wing subjected to engine thrust. In Advanced Materials Research II (pp. 1568-1572). (Advanced Materials Research; Vol. 463-464). https://doi.org/10.4028/www.scientific.net/AMR.463-464.1568
Amoozgar, Mohammad Reza ; Irani, Saied. / Bending-torsional flutter of a composite rectangular cantilever wing subjected to engine thrust. Advanced Materials Research II. 2012. pp. 1568-1572 (Advanced Materials Research).
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abstract = "The bending-torsional flutter characteristics of a cantilever composite wing subjected to engine thrust are presented. The engine thrust modeled as a follower force and the wing modeled as a two degree of freedom beam. In order to consider the spanwise and chordwise location and the properties of the engine location, the generalized function theory is used. Unsteady Theodorsen aerodynamic theory in time domain, is used. The general laminate composite theory is used for modeling the effects of the ply angles on the flutter boundary. The Ritz method is subsequently applied to convert the partial differential equations into a set of ordinary differential equations. In order to precisely consider the location of the engine Dirac delta function is used. Moreover, the numerical results are compared with the published results and excellent agreement is observed. Numerical results highlighting the effect of engine thrust on the wing instability, is presented.",
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Amoozgar, MR & Irani, S 2012, Bending-torsional flutter of a composite rectangular cantilever wing subjected to engine thrust. in Advanced Materials Research II. Advanced Materials Research, vol. 463-464, pp. 1568-1572, 2nd International Conference on Advanced Material Research, Chengdu, China, 7/01/12. https://doi.org/10.4028/www.scientific.net/AMR.463-464.1568

Bending-torsional flutter of a composite rectangular cantilever wing subjected to engine thrust. / Amoozgar, Mohammad Reza; Irani, Saied.

Advanced Materials Research II. 2012. p. 1568-1572 (Advanced Materials Research; Vol. 463-464).

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

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