Research data supporting "Design Study for a Laminar-Flying-Wing Aircraft": Structure Loads - spanwise aerodynamic loads on the lifting surfaces of the aircraft
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Type
Dataset
Change log
Authors
Saeed, T. I.
Graham, W. R.
Description
AVL output files providing spanwise aerodynamic loads on the lifting surfaces of the aircraft. For the competitor (files starting 'conv'), these are the wing, stabiliser and fin.
Version
Software / Usage instructions
Keywords
Publisher
Rights
Sponsorship
This work was supported by the Engineering and Physical Sciences Council