Research data supporting "Design Study for a Laminar-Flying-Wing Aircraft": Surface Pressures - LFW aerofoil surface pressure coefficients in the form used for the suction calculation
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Dataset
Change log
Authors
Saeed, T. I.
Graham, W. R.
Description
These files provide the LFW aerofoil surface pressure coefficients in the form used for the suction calculation. 'Geom' files give the section geometry (standard, chord-normalised, coordinates) in two alternative orderings; 'LoCp' and 'UpCp' give pressure coefficient as function of (normalised) chordwise distance for pressure and suction surfaces respectively. For case listing, see 'nameConvention.txt'.
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Sponsorship
This work was supported by the Engineering and Physical Sciences Council