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- Fachbereich Luft- und Raumfahrttechnik (192) (remove)
The impact of wake model effects is investigated for two highly
non-planar lifting systems. Dependent on the geometrical
arrangement of the configuration, the wake model shape is found
to considerably affect the estimation. Particularly at higher angles
of attack, an accurate estimation based on the common linear wake
model approaches is involved.
Wing weight estimation methodology for highly non-planar lifting systems during conceptual design
(2013)
Euler-based induced drag estimation for highly non-planar lifting systems during conceptional design
(2013)