airfoil.scad

poly_airfoil=[[0.001,0.000],[0.000,0.006],[0.000,0.014],[0.000,0.018],[0.001,0.023],[0.002,0.029],[0.003,0.034],[0.004,0.041],[0.006,0.047],[0.009,0.054],[0.012,0.060],[0.016,0.067],[0.020,0.074],[0.026,0.081],[0.032,0.088],[0.039,0.094],[0.042,0.098],[0.051,0.104],[0.055,0.107],[0.060,0.110],[0.065,0.113],[0.070,0.116],[0.076,0.119],[0.082,0.121],[0.088,0.124],[0.095,0.127],[0.101,0.129],[0.109,0.131],[0.116,0.133],[0.124,0.135],[0.132,0.137],[0.140,0.139],[0.149,0.140],[0.158,0.141],[0.168,0.142],[0.178,0.143],[0.188,0.144],[0.199,0.145],[0.210,0.145],[0.221,0.145],[0.233,0.145],[0.250,0.145],[0.266,0.144],[0.283,0.143],[0.301,0.142],[0.318,0.141],[0.336,0.139],[0.355,0.137],[0.374,0.135],[0.393,0.133],[0.412,0.130],[0.453,0.124],[0.474,0.121],[0.496,0.117],[0.541,0.109],[0.588,0.100],[0.638,0.089],[0.690,0.077],[0.746,0.064],[0.804,0.050],[0.866,0.035],[0.931,0.018],[1.000,0.000],[0.001,0.000]];