Publisher: Cambridge University Press
E-ISSN: 2059-6464|118|1206|861-901
ISSN: 0001-9240
Source: The Aeronautical Journal, Vol.118, Iss.1206, 2014-08, pp. : 861-901
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
A wind-tunnel based study of helicopter tail rotor blade vortex interaction
The Aeronautical Journal, Vol. 108, Iss. 1083, 2004-05 ,pp. :
Effects of rotor blade-tip geometry on helicopter trim and control response
The Aeronautical Journal, Vol. 121, Iss. 1239, 2017-05 ,pp. :