HS1712 Airfoil

HS1 family of prop airfoils

HS1712 Airfoil (x,y) Co-ordinates

0 0.00001
0.0005 0.0043
0.001 0.006
0.002 0.00903
0.003 0.01127
0.005 0.0149
0.0075 0.01861
0.01 0.0218
0.02 0.03186
0.03 0.03967
0.04 0.04688
0.05 0.05192
0.06 0.05698
0.07 0.0611
0.08 0.06562
0.09 0.06937
0.1 0.0728
0.12 0.07886
0.14 0.08401
0.16 0.08839
0.18 0.09211
0.2 0.09525
0.22 0.09786
0.24 0.1
0.26 0.10173
0.28 0.10313
0.3 0.10418
0.34 0.10542
0.36 0.10632
0.38 0.10687
0.4 0.107
0.44 0.10656
0.46 0.106
0.48 0.10526
0.5 0.10423
0.54 0.10154
0.56 0.09965
0.58 0.09795
0.6 0.09587
0.64 0.09125
0.66 0.08872
0.68 0.08605
0.7 0.08322
0.74 0.07789
0.76 0.07477
0.78 0.07028
0.8 0.06668
0.82 0.06262
0.84 0.05834
0.86 0.05368
0.88 0.04856
0.9 0.04299
0.91 0.03997
0.92 0.03686
0.93 0.03364
0.94 0.03032
0.95 0.02689
0.96 0.02335
0.97 0.01968
0.98 0.0157
0.99 0.01171
1 0.0072
1 -0.0107
0.99 -0.00976
0.98 -0.00882
0.97 -0.00829
0.96 -0.00807
0.95 -0.00785
0.94 -0.00753
0.93 -0.00742
0.92 -0.00721
0.91 -0.00701
0.9 -0.00683
0.88 -0.00653
0.86 -0.00633
0.84 -0.00621
0.82 -0.00614
0.8 -0.00611
0.78 -0.00609
0.76 -0.00611
0.74 -0.00619
0.7 -0.00658
0.68 -0.00687
0.66 -0.00721
0.64 -0.00756
0.6 -0.00824
0.58 -0.00856
0.56 -0.00888
0.54 -0.00919
0.5 -0.00985
0.48 -0.0102
0.46 -0.0106
0.44 -0.01105
0.4 -0.01216
0.38 -0.01279
0.36 -0.01344
0.34 -0.01389
0.3 -0.01536
0.28 -0.01607
0.26 -0.01688
0.24 -0.01786
0.22 -0.01901
0.2 -0.0203
0.18 -0.02159
0.16 -0.02279
0.14 -0.02374
0.12 -0.0244
0.1 -0.02469
0.09 -0.02466
0.08 -0.0245
0.07 -0.02417
0.06 -0.02353
0.05 -0.02283
0.04 -0.02109
0.03 -0.02006
0.02 -0.01767
0.01 -0.01376
0.0075 -0.0123
0.005 -0.01044
0.003 -0.00842
0.002 -0.00709
0.001 -0.00519
0.0005 -0.00377
0 0

HS1712 Airfoil CAD files

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