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SP2_geom.dat
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SP2_geom.dat
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Variables = "r [m]", "chord [m]", "twist [deg]", "total rake [m]", "skew [deg]" Twist ref. is located at mid chord. Blade section: NACA4412 airfoil which params are rebuilt from CAD planar sections
9.0000000e-03 1.0174790e-02 3.8066434e+01 4.8251748e-05 -3.4806294e+00
1.1040816e-02 1.1850344e-02 4.0447791e+01 8.6764256e-05 -3.4045517e+00
1.3081633e-02 1.3162700e-02 4.2122807e+01 1.2514085e-04 -3.3275757e+00
1.5122449e-02 1.4167062e-02 4.3184194e+01 1.6338152e-04 -3.2505098e+00
1.7163265e-02 1.4913918e-02 4.3717519e+01 2.0148627e-04 -3.1740942e+00
1.9204082e-02 1.5449213e-02 4.3801466e+01 2.3945510e-04 -3.0990016e+00
2.1244898e-02 1.5814513e-02 4.3508092e+01 2.7728802e-04 -3.0258364e+00
2.3285714e-02 1.6047170e-02 4.2903089e+01 3.1498501e-04 -2.9551351e+00
2.5326531e-02 1.6180495e-02 4.2046038e+01 3.5254609e-04 -2.8873666e+00
2.7367347e-02 1.6243920e-02 4.0990674e+01 3.8997125e-04 -2.8229315e+00
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3.1448980e-02 1.6260412e-02 3.8472243e+01 4.6441382e-04 -2.7053247e+00
3.3489796e-02 1.6254461e-02 3.7089724e+01 5.0143122e-04 -2.6526149e+00
3.5530612e-02 1.6260905e-02 3.5670502e+01 5.3831271e-04 -2.6041621e+00
3.7571429e-02 1.6292296e-02 3.4242944e+01 5.7505828e-04 -2.5600275e+00
3.9612245e-02 1.6358311e-02 3.2831120e+01 6.1166792e-04 -2.5202042e+00
4.1653061e-02 1.6465917e-02 3.1455060e+01 6.4814165e-04 -2.4846173e+00
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5.1857143e-02 1.7703209e-02 2.5562164e+01 8.2847153e-04 -2.3628580e+00
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1.0491837e-01 7.1039199e-03 1.2510049e+01 1.7114117e-03 7.5641621e-02
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