Static aeroelastic optimisation to wing structural weight estimation of an extremely manoeuvrable UAV

Publisher: Cambridge University Press

E-ISSN: 2059-6464|119|1218|1033-1043

ISSN: 0001-9240

Source: The Aeronautical Journal, Vol.119, Iss.1218, 2015-08, pp. : 1033-1043

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract