Author: FeiChengweiSchool of Jet and Propulsion Beihang University Beijing China. TangWenzhongSchool of Computer Science and Engineering Beihang University Beijing China. BaiGuangchenSchool of Jet and Propulsion Beihang University Beijing China. ShuangSchool of Life Science Beijing Normal University Beijing China.
Publisher: Emerald Group Publishing Ltd
ISSN: 0002-2667
Source: Aircraft Engineering, Vol.87, Iss.4, 2015-07, pp. : 312-321
Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.
Abstract
Related content
Main Rotor Blade Design and Development
Journal of the American Helicopter Society, Vol. 4, Iss. 4, 1959-10 ,pp. :
Blade Design for Reduced Helicopter Vibration
Journal of the American Helicopter Society, Vol. 28, Iss. 3, 1983-07 ,pp. :
A New Approach to Rotor Blade Dynamic Analysis
By Berman Alex
Journal of the American Helicopter Society, Vol. 10, Iss. 3, 1965-07 ,pp. :