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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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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This work was supported by the Engineering and Physical Sciences Council