[1]
|
Kesel, A.B., Philippiand, U. and Nachtigall, W. (1998) Biomechanical Aspects of the Insect Wing: An Analysis Using the Finite Element Method. Computers in Biology and Medicine, 28, 423-437.
http://dx.doi.org/10.1016/S0010-4825(98)00018-3
|
[2]
|
Yu, C., Ang, H., Chen, Q., et al. (2008) Three-Dimension Un-steady Vortex Lattice Method for Flexible Structure Flapping-Wing Aerial Vehicle. Journal of Nanjing University of Aeronautics and Astronautics, 40, 451-455.
|
[3]
|
Yu, C., Ang, H., Yi, K., et al. (2009) The Study of Deformation for Membrane Flapping-Wing Aerial Vehicles. Chinese Journal of Computational Mechanics, 26, 935-941.
|
[4]
|
Fitzgerald, C., Valdez, M. and Balachandran, B. (2011) A Comparison of Computational Models for Fluid-Structure Interaction Studies of Flexible Flapping Wing Systems. The 49th AIAA Aerospace Sciences Meeting, Orlando, 4-7 January 2011.
|
[5]
|
Nakata, T. and Liu, H. (2012) A Fluid-Structure Interaction Model of Insect Flight with Flexible Wings. Journal of Computational Physics, 231, 1822-1847. http://dx.doi.org/10.1016/j.jcp.2011.11.005
|
[6]
|
Stewart, E., Patil, M., Canfield, R. and Snyder, R. (2014) Aeroelastic Shape Optimization of a Flapping Wing. The 10th AIAA Multidisciplinary Design Optimization Conference, National Harbor, 13-17 January 2014.
http://dx.doi.org/10.2514/6.2014-0469
|
[7]
|
Vincent, J.F. (1980) Insect Cuticle: A Paradigm for Natural Composites. Symposia of the Society for Experimental Biology, 34, 183-210.
|
[8]
|
Cho, H., Kwak, J. and Shin, S. (2014) Computa-tional Analysis for Flapping Wing by Coupling the Geometrically Exact Beam and Preconditioned Navier-Stokes So-lution. The 55th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, National Harbor, 13-17 January 2014.
|
[9]
|
Mason, J., Jennings, A. and Black, J. (2013) Validation of a Finite Analysis of a Flapping Wing against Inertial and Aeroelastic Responses. The 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Boston, 8-11 April 2013.
|
[10]
|
He, H., Zhou, X., Long, Y. and Yu, C. (2010) Improved UVLM for Flapping-Wing Aerodynamics Computation. Transactions of Nanjing University of Aeronautics & Astronautics, 27, 205-212.
|
[11]
|
Yu, Y., Yang, Q. and Wang, X. (2013) Finite Element Analysis of Fluid-Structure Interaction for the Design of MAV Aerodynamic Shape. Computers & Fluids, 76, 50-57. http://dx.doi.org/10.1016/j.compfluid.2013.01.026
|
[12]
|
Lian, Y. and Shyy, W. (2003) Three-Dimensional Fluid-Struture Interactions of a Membrane Wing for Micro Air Vehicle Applications. The 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Norfolk, 7-10 April 2003.
|
[13]
|
Combes, S.A. and Daniel, T.L. (2003) Flexural Stiffness in Insectwings: I. Scaling and the Influence of Wing Venation. Journal of Experimental Biology, 206, 2979-2987. http://dx.doi.org/10.1242/jeb.00523
|
[14]
|
Combes, S.A. and Daniel, T.L. (2003) Flexural Stiffness in Insectwings: II. Spatial Distribution and Dynamic Wing Bending. Journal of Experimental Biology, 206, 2989-2997. http://dx.doi.org/10.1242/jeb.00524
|
[15]
|
Bao, L., Hu, J., Yu, Y., et al. (2006) Viscoelastic Constitutive Model Related to Deformation of Insect Wing under Loading in Flapping Motion. Applied Mathematics and Mechanics, 27, 741-748.
http://dx.doi.org/10.1007/s10483-006-0604-1
|