foil_mises84.m

%
% Author: Michael J. Fairchild (Princeton University)
% Date: 2016-09-24
%
function f = foil_mises84()
le = 26;
data = [
   1.0000000e+00   0.0000000e+00 ; ...
   9.9485800e-01   7.8200000e-04 ; ...
   9.8086600e-01   2.7840000e-03 ; ...
   9.5888400e-01   5.7210000e-03 ; ...
   9.2953600e-01   9.3510000e-03 ; ...
   8.9345500e-01   1.3459000e-02 ; ...
   8.5130800e-01   1.7837000e-02 ; ...
   8.0381500e-01   2.2285000e-02 ; ...
   7.5175000e-01   2.6618000e-02 ; ...
   6.9594600e-01   3.0671000e-02 ; ...
   6.3726600e-01   3.4289000e-02 ; ...
   5.7661700e-01   3.7341000e-02 ; ...
   5.1491500e-01   3.9712000e-02 ; ...
   4.5309500e-01   4.1314000e-02 ; ...
   3.9208200e-01   4.2083000e-02 ; ...
   3.3279100e-01   4.1979000e-02 ; ...
   2.7610500e-01   4.0979000e-02 ; ...
   2.2286500e-01   3.9096000e-02 ; ...
   1.7386100e-01   3.6360000e-02 ; ...
   1.2981900e-01   3.2820000e-02 ; ...
   9.1393000e-02   2.8555000e-02 ; ...
   5.9146000e-02   2.3651000e-02 ; ...
   3.3560000e-02   1.8220000e-02 ; ...
   1.5008000e-02   1.2379000e-02 ; ...
   3.7670000e-03   6.2590000e-03 ; ...
   0.0000000e+00   0.0000000e+00 ; ...
   3.7670000e-03  -6.2590000e-03 ; ...
   1.5010000e-02  -1.2379000e-02 ; ...
   3.3560000e-02  -1.8220000e-02 ; ...
   5.9146000e-02  -2.3651000e-02 ; ...
   9.1393000e-02  -2.8555000e-02 ; ...
   1.2981900e-01  -3.2820000e-02 ; ...
   1.7386100e-01  -3.6360000e-02 ; ...
   2.2286500e-01  -3.9096000e-02 ; ...
   2.7610500e-01  -4.0979000e-02 ; ...
   3.3297400e-01  -4.1979000e-02 ; ...
   3.9208400e-01  -4.2083000e-02 ; ...
   4.5309800e-01  -4.1314000e-02 ; ...
   5.1491800e-01  -3.9712000e-02 ; ...
   5.7662000e-01  -3.7341000e-02 ; ...
   6.3727100e-01  -3.4289000e-02 ; ...
   6.9594800e-01  -3.0671000e-02 ; ...
   7.5175300e-01  -2.6618000e-02 ; ...
   8.0381500e-01  -2.2285000e-02 ; ...
   8.5130800e-01  -1.7837000e-02 ; ...
   8.9345500e-01  -1.3459000e-02 ; ...
   9.2953600e-01  -9.3510000e-03 ; ...
   9.5888400e-01  -5.7210000e-03 ; ...
   9.8086600e-01  -2.7840000e-03 ; ...
   9.9485800e-01  -7.8200000e-04 ; ...
   1.0000000e+00   0.0000000e+00 ; ...
];
f = Airfoil2d(data(:,1),data(:,2),le);