Applied Mathematics and Mechanics >
VISCOELASTIC CONSTITUTIVE MODEL RELATED TO DEFORMATION OF INSECT WING UNDER LOADING IN FLAPPING MOTION
Received date: 2005-10-17
Revised date: 2006-02-10
Online published: 2006-06-18
Supported by
null
Key words: null
BAO Lin;HU Jin-song;YU Yong-liang;CHENG Peng;XU Bo-qing;TONG Bing-gang . VISCOELASTIC CONSTITUTIVE MODEL RELATED TO DEFORMATION OF INSECT WING UNDER LOADING IN FLAPPING MOTION[J]. Applied Mathematics and Mechanics, 2006 , 27(6) : 741 -748 . DOI: 10.1007/s10483-006-0604-1
null
/
| 〈 |
|
〉 |