HOR07 airfoil

Onera propeller blade airfoils from US Patent 4,773,825

HOR07 airfoil (x,y) Co-ordinates

0 0
0.003773 0.008671
0.00904 0.014252
0.014225 0.017769
0.021437 0.021708
0.026576 0.024189
0.03222 0.026756
0.035803 0.028218
0.041616 0.030503
0.04646 0.03234
0.056549 0.035851
0.066638 0.03913
0.074678 0.041625
0.084785 0.044712
0.094963 0.047639
0.1052 0.050404
0.115476 0.053007
0.125779 0.054976
0.136122 0.056935
0.146511 0.0599
0.156884 0.061859
0.167242 0.06281
0.177626 0.064768
0.18801 0.066727
0.198403 0.068685
0.224553 0.071566
0.245079 0.073873
0.295448 0.076422
0.345806 0.077158
0.396155 0.076082
0.446497 0.073697
0.496832 0.070204
0.54716 0.065301
0.597484 0.059491
0.647803 0.052977
0.698119 0.045858
0.748437 0.038941
0.798755 0.032125
0.849071 0.025107
0.89939 0.018492
0.919517 0.015665
0.949708 0.011575
0.969835 0.008848
0.989963 0.006222
1.000026 0.004909
0.999974 -0.004909
0.99494 -0.00448
0.989907 -0.00414
0.97984 -0.003391
0.959705 -0.002075
0.939571 -0.000657
0.919436 0.000559
0.899303 0.002178
0.8691 0.004052
0.848965 0.005369
0.828831 0.006685
0.798627 0.008459
0.758355 0.010589
0.728151 0.012161
0.697945 0.013431
0.65767 0.014957
0.627461 0.015723
0.597251 0.016188
0.556969 0.016404
0.526757 0.016566
0.49654 0.015722
0.456252 0.014931
0.426034 0.014086
0.395817 0.013242
0.375665 0.011336
0.355519 0.010437
0.335372 0.009639
0.315223 0.008236
0.295072 0.006532
0.257147 0.003211
0.232209 0.000827
0.207179 -0.001828
0.197102 -0.002922
0.187015 -0.004006
0.176918 -0.00507
0.166802 -0.006123
0.156705 -0.007166
0.146608 -0.0082
0.136482 -0.009213
0.126315 -0.010216
0.116108 -0.011188
0.10564 -0.011887
0.095565 -0.01274
0.08549 -0.013441
0.07441 -0.013855
0.065345 -0.013987
0.053261 -0.013922
0.043191 -0.013667
0.033123 -0.013109
0.02809 -0.01277
0.023057 -0.012199
0.018026 -0.011457
0.012996 -0.010423
0.00811 -0.008896
0.003168 -0.006372
0 0

HOR07 airfoil CAD files

DOWNLOAD FROM HERE

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