@inproceedings{e17b43fcf7204efbbc4a44362d1970b7,
title = "Computational fluid-structure dynamics coupling research of flexible wing",
abstract = "This paper presents a computational fluid-structure dynamics coupling method of flexible wing. The computational fluid dynamics is solving RANS equations. The stiffness used in computational structure dynamics is tested by experiments. Then the aerodynamic performance of flexible wing is researched and compared with rigid wing. The results show that the lift and thrust generated by flexible wing are less than the rigid wing. Flexible wing can slower the variety of aerodynamic performance when the flight environment is changing. And flexible wing has bigger stalling angle.",
keywords = "Aerodynamic performance, CFSD, Flexible wing, MAV",
author = "Yang, {Wen Qing} and Song, {Bi Feng} and Song, {Wen Ping} and Li, {Zhan Ke} and Zhang, {Ya Feng}",
year = "2012",
doi = "10.4028/www.scientific.net/AMR.354-355.655",
language = "英语",
isbn = "9783037852668",
series = "Advanced Materials Research",
pages = "655--658",
booktitle = "Progress in Power and Electrical Engineering",
note = "2011 International Conference on Energy, Environment and Sustainable Development, ICEESD 2011 ; Conference date: 21-10-2011 Through 23-10-2011",
}