Publisher： Cambridge University Press
E-ISSN： 2059-6464|108|1080|75-84
ISSN： 0001-9240
Source： The Aeronautical Journal, Vol.108, Iss.1080, 2004-02, pp. : 75-84
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
Parallel adjoint-based optimisation of a blended wing body aircraft with shock control bumps
The Aeronautical Journal, Vol. 111, Iss. 1117, 2007-03 ,pp. :
Access to resources
Recommend
Blended wing body structural concept development
The Aeronautical Journal, Vol. 114, Iss. 1158, 2010-08 ,pp. :
Relationships between flying qualities and flight tests parameters for the F/A-18 aircraft
The Aeronautical Journal, Vol. 111, Iss. 1118, 2007-04 ,pp. :