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The Bezier interpolation is introduced as a new discretization method for the rotating flexible beam deformation. First, the model of the rotating flexible beam is built. Then, the rigid-flexible coupling dynamic equations are established via employing the second kind of Lagrange's equation. The longitudinal deformation and the transverse deformation of the flexible beam are considered, and the coupling term of the deformation which is caused by the transverse deformation is included in the total longitudinal deformation; and a software package for the dynamics simulation of the flexible beam is developed. Finally, the simulation results of the Bezier interpolation are compared with those of the assumed method and the finite element method. Simulation results demonstrate that the computational efficiency of the Bezier interpolation is the highest, the computational accuracy of Bezier interpolation is in accordance with the needs of engineering, and is higher than the one of assumed mode method in high-speed case. The Bezier interpolation method is better than the assumed mode method in dealing with the large deformation dynamics problem. So the Bezier interpolation method will be hopeful to win popularity in the field of multi-body system dynamics.
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Keywords:
- flexible beam /
- Bezier interpolation /
- natural frequency /
- natural vibration mode
[1] [2] Eraman A G, Sandor G N 1972 Mech Mach Theory. 7 19
[3] [4] Lowenm G G, Jandrasits W G 1972 Mech Mach Theory. 7 3
[5] Fang J S, Zhang D G 2013 Acta Phys. Sin. 62 044501 (in Chinese) [方建士, 章定国 2013 62 044501]
[6] [7] He X S, Deng F Y, Wu G Y, Wang R 2010 Acta Phys. Sin. 59 25 (in Chinese) [和兴锁, 邓峰岩, 吴根勇, 王睿 2010 59 25]
[8] [9] He X S, Deng F Y, Wang R 2010 Acta Phys. Sin. 59 1428 (in Chinese) [和兴锁, 邓峰岩, 王睿 2010 59 1428]
[10] [11] He X S, Song M, Deng F Y 2011 Acta Phys. Sin. 60 044501 (in Chinese) [和兴锁, 宋明, 邓峰岩 2011 60 044501]
[12] [13] Valembois R E, Fisette P, Samin J C 1997 Nonlinear Dyn. 12 367
[14] [15] [16] Lin H W, Liu L G, Wang G J 2002 Comput Aided Design. 34 637
[17] Oh M J, Suthunyatanakit K, Park S H, Kim T W 2012 Comput Aided Design. 44 671
[18] [19] Xu G, Wang G Z, Chen W Y 2011 Sci China Inform Sci. 54 1395
[20] [21] [22] Sanborn G G, Shabana A A 2009 Multibody Syst Dyn. 22 181
[23] [24] Sanborn G G, Shabana A A 2009 Nonlinear Dyn. 58 565
[25] [26] Lan P, Shabana A A 2010 J Vib Acoust. 132 041007
[27] [28] Lan P, Shabana A A 2010 Nolinear Dyn. 61 193
[29] [30] He X S Li X H, Deng F Y 2011 Acta Phys. Sin. 60 024502 (in Chinese) [和兴锁, 李雪华, 邓峰岩 2011 60 024502]
[31] Hu H Y 2005 Mechanical Vibration (Beijing: Beijing University of Aeronautics and Astronautics Press) p105 (in Chinese) [胡海岩2005机械振动基础(北京: 北京航空航天大学出版社)第105页]
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[1] [2] Eraman A G, Sandor G N 1972 Mech Mach Theory. 7 19
[3] [4] Lowenm G G, Jandrasits W G 1972 Mech Mach Theory. 7 3
[5] Fang J S, Zhang D G 2013 Acta Phys. Sin. 62 044501 (in Chinese) [方建士, 章定国 2013 62 044501]
[6] [7] He X S, Deng F Y, Wu G Y, Wang R 2010 Acta Phys. Sin. 59 25 (in Chinese) [和兴锁, 邓峰岩, 吴根勇, 王睿 2010 59 25]
[8] [9] He X S, Deng F Y, Wang R 2010 Acta Phys. Sin. 59 1428 (in Chinese) [和兴锁, 邓峰岩, 王睿 2010 59 1428]
[10] [11] He X S, Song M, Deng F Y 2011 Acta Phys. Sin. 60 044501 (in Chinese) [和兴锁, 宋明, 邓峰岩 2011 60 044501]
[12] [13] Valembois R E, Fisette P, Samin J C 1997 Nonlinear Dyn. 12 367
[14] [15] [16] Lin H W, Liu L G, Wang G J 2002 Comput Aided Design. 34 637
[17] Oh M J, Suthunyatanakit K, Park S H, Kim T W 2012 Comput Aided Design. 44 671
[18] [19] Xu G, Wang G Z, Chen W Y 2011 Sci China Inform Sci. 54 1395
[20] [21] [22] Sanborn G G, Shabana A A 2009 Multibody Syst Dyn. 22 181
[23] [24] Sanborn G G, Shabana A A 2009 Nonlinear Dyn. 58 565
[25] [26] Lan P, Shabana A A 2010 J Vib Acoust. 132 041007
[27] [28] Lan P, Shabana A A 2010 Nolinear Dyn. 61 193
[29] [30] He X S Li X H, Deng F Y 2011 Acta Phys. Sin. 60 024502 (in Chinese) [和兴锁, 李雪华, 邓峰岩 2011 60 024502]
[31] Hu H Y 2005 Mechanical Vibration (Beijing: Beijing University of Aeronautics and Astronautics Press) p105 (in Chinese) [胡海岩2005机械振动基础(北京: 北京航空航天大学出版社)第105页]
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