Publisher： Cambridge University Press
E-ISSN： 2059-6464|108|1081|117-124
ISSN： 0001-9240
Source： The Aeronautical Journal, Vol.108, Iss.1081, 2004-03, pp. : 117-124
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
Nonlinear identification and control of aircraft
International Journal of Systems Science, Vol. 31, Iss. 8, 2000-08 ,pp. :
Access to resources
Recommend
Efficient optimisation of large aircraft fuselage structures
The Aeronautical Journal, Vol. 118, Iss. 1199, 2014-01 ,pp. :
On the effectiveness of active aeroelastic structures for morphing aircraft
The Aeronautical Journal, Vol. 117, Iss. 1197, 2013-11 ,pp. :
Benefits and design challenges of adaptive structures for morphing aircraft
The Aeronautical Journal, Vol. 110, Iss. 1105, 2006-03 ,pp. :
On the dynamics of rotating and rolling structures
Archive of Applied Mechanics, Vol. 78, Iss. 6, 2008-06 ,pp. :