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VIEW THE ORIGINAL ARTICLEPublication: Journal of Aerospace Engineering
Volume 25, Issue 3
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References
Bisplinghoff, R. L., Ashley, H., and Halfman, R. L. (1996). Aeroelasticity. Dover, New York.
Goland, M. (1945). “The flutter of a uniform cantilever wing.” J. Appl. Mech.JAMCAV, 12, 197–208.
Hodges, D. H., Patil, M. J., and Chae, S. (2002). “Effect of thrust on bendingtorsion flutter of wings.” J. Aircr.JAIRAM, 39(2), 371–376.
Hodges, D. H., and Pierce, G. A. (2002). Introduction to structural dynamics and aeroelasticity, Cambridge University Press, Cambridge, U.K.
Karpouzian, C., and Librescu, L (1996). “Non-classical effects on divergence and flutter of anisotropic swept aircraft wings.” AIAA J.AIAJAH, 34(4), 786–794.
Peters, D. A., Karunamoorthy, S., and Cao, W. M. (1995). “Finite state induced flow models: Part I: Two-dimensional thin airfoil.” J. Aircr.JAIRAM, 32, 313–322.
Information & Authors
Information
Published In
Journal of Aerospace Engineering
Volume 25 • Issue 3 • July 2012
Pages: 474 - 476
Copyright
© 2012. American Society of Civil Engineers.
History
Received: Feb 10, 2011
Accepted: Jun 1, 2011
Published online: Jun 15, 2012
Published in print: Jul 1, 2012
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Authors
Affiliations
Assistant Professor, Dept. of Aerospace Engineering, Sharif Univ. of Technology, P.O. Box 11155-8639, Tehran, Iran (corresponding author). E-mail: [email protected]
P. Zarifian
Research Fellow, Dept. of Aerospace Engineering, Sharif Univ. of Technology, Tehran, Iran.
A. R. Askarian
Faculty of Mechanical Engineering Dept., Vali-e-Asr Univ., P.O. Box 77139-36417, Rafsanjan, Iran.
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