Author: Zhou Hao Rahman Tawfiqur Chen Wanchun
Publisher: Emerald Group Publishing Ltd
ISSN: 0002-2667
Source: Aircraft Engineering, Vol.87, Iss.5, 2015-09, pp. : 454-464
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
Simulation methodology for high velocity impact in composite aircraft structures
By Johnson A.
Air & Space Europe, Vol. 3, Iss. 3, 2001-05 ,pp. :
Precision Guidance for Steep Angle Approach and Landing
Journal of the American Helicopter Society, Vol. 14, Iss. 4, 1969-10 ,pp. :