G.R. Ye
Zhejiang University
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Publication
Featured researches published by G.R. Ye.
AIAA Journal | 2003
W.Q. Chen; J.B. Cai; G.R. Ye
State-space approach is developed to analyze the bending and free vibration of a simply supported, cross-ply laminated rectangular plate featuring interlaminar bonding imperfections, for which a general linear spring layer model is adopted. The analysis is directly based on the three-dimensional theory of orthotropic elasticity and is completely exact. Numerical comparison is made, showing that although the plate theory developed in the literature behaves well for moderately thick perfect laminates it can become inaccurate when bonding imperfections are present. The special problem of the laminate in cylindrical bending is also considered, and the validity of the assumption of cylindrical bending is investigated through numerical examples.
AIAA Journal | 2004
Weiqiu Chen; J. Ying; J.B. Cai; G.R. Ye
3Shyy, W., Udaykumar, H. S., Rao, M. M., and Smith, R. W., Computational Fluid Dynamics with Moving Boundaries, Taylor and Francis, Philadelphia, 1996, pp. 31, 32. 4Jackson, P. S., and Christie, G. W., “Numerical Analysis of ThreeDimensional Elastic Membrane Wings,” AIAA Journal, Vol. 25, 1987, pp. 676–682. 5Lian, Y., Shyy, W., Ifju, P. G., and Verron, E., “Membrane Wing Model for Micro Air Vehicles,” AIAA Journal, Vol. 41, No. 12, 2003, pp. 2492–2494. 6Hutchison, M. G., Unger, E. R., Mason, W. H., Grossman, B., and Haftka, R. T., “Variable-Complexity Aerodynamic Optimization of a High-Speed Civil Transport Wing,” Journal of Aircraft, Vol. 31, 1994, pp. 110–116. 7Burgee, S., Giunta, A. A., Narducci, R., Watson, L. T., Grossman, B., and Haftka, R. T., “A Coarse Grained Parallel Variable-Complexity Multidisciplinary Optimization Paradigm,” International Journal of Supercomputer Applications and High Performance Computing, Vol. 10, 1996, pp. 269–299. 8Mason, B. H., Haftka, R. T., Johnson, E. R., and Farley, G. L., “Variable Complexity Design of Composite Fuselage Frames by Response Surface Techniques,” Thin Wall Structures, Vol. 32, 1998, pp. 235–261. 9Knill, D. L., Giunta, A. A., Baker, C. A., Grossman, B., Mason, W. H., Haftka, R. T., and Watson, L.T., “Response Surface Methods Combining Linear and Euler Aerodynamics for Supersonic Transport Design,” Journal of Aircraft, Vol. 36, 1999, pp. 75–86. 10Design Optimization Tools, Vanderplaats Research and Development, Inc., Colorado Springs, CO, 1999. 11Lian, Y., Shyy, W., and Haftka, R. T., “Shape Optimization of a Membrane Wing for Micro Air Vehicles,” AIAA Paper 2003-0106, Jan. 2003. 12Duchon, J. P., “Splines Minimizing Rotation-Invariant Semi-Norms in Sobolev Spaces,” Constructive Theory of Functions of Several Variables, edited by W. Schempp and K. Zeller, Springer-Verlag, Berlin, 1977, pp. 85–100. A. Plotkin Associate Editor
International Journal of Solids and Structures | 2004
W.Q. Chen; Jiachang Cai; G.R. Ye; Y.F. Wang
International Journal of Solids and Structures | 2004
W.Q. Chen; Y.F. Wang; Jiachang Cai; G.R. Ye
Archive of Applied Mechanics | 2002
W.Q. Chen; Yunhao Lu; G.R. Ye; J.B. Cai
Mechanics Research Communications | 2001
G.R. Ye; Wei Chen; J.B. Cai
Computers & Structures | 2004
W.Q. Chen; J Ying; Jiachang Cai; G.R. Ye
Composites Science and Technology | 2004
Jiachang Cai; W.Q. Chen; G.R. Ye
Journal of Sound and Vibration | 2000
J.B. Cai; Wei Chen; G.R. Ye; Haojiang Ding
Computer Methods in Applied Mechanics and Engineering | 2005
W.Q. Chen; J.B. Cai; G.R. Ye