Closure to “Robust Aeroelastic Control of a Thin-Walled Wing Structure with Model Uncertainty” by Jeonghwan Choo, Gwonchan Yoon, Ji-Seok Song, Taeyun Kwon, Sungsoo Na, and Zhanming Qin
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Volume 27, Issue 1
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References
Librescu, L., and Song, O. (1991). “Behavior of thin-walled beams made of advanced composite materials and incorporating non-classical effects.” Appl. Mech. Rev., 44(11S), S174–S180.
Na, S., Song, J.-S., Choo, J.-H., and Qin, Z. (2011). “Dynamic aeroelastic response and active control of composite thin-walled beam structures in compressible flow.” J. Sound Vibrat., 330(21), 4998–5013.
Qin, Z. (2001). “Vibration and aeroelasticity of advanced aircraft wings modeled as thin-walled beams.” Ph.D. thesis, Virginia Polytechnic Institute and State Univ., Blacksburg, VA.
Qin, Z., and Librescu, L. (2002). “On a shear-deformable theory of anisotropic thin-walled beams: Further contribution and validation.” Compos. Struct., 56(4), 345–358.
Qin, Z., Librescu, L., and Marzocca, P. (2003). “Aeroelasticity of composite aerovehicle wings in supersonic flows.” J. Spacecr. Rockets, 40(2), 162–173.
Qin, Z., Marzocca, P., and Librescu, L. (2002). “Aeroelastic instability and response of advanced aircraft wings at subsonic flight speeds.” Aerosp. Sci. Technol., 6(3), 195–208.
Rehfield, L., and Atilgan, A. (1989). “Shear center and elastic axis and their usefulness for composite thin-walled beams.” Proc., 4th American Society for Composites Technical Conf. on Composite Materials, Technomics, Technomic Publishing Company, Lancaster, PA.
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Published In
Journal of Aerospace Engineering
Volume 27 • Issue 1 • January 2014
Pages: 194 - 195
Copyright
© 2014 American Society of Civil Engineers.
History
Received: Jan 14, 2013
Accepted: Mar 11, 2013
Published online: Dec 16, 2013
Published in print: Jan 1, 2014
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