HS1708 Airfoil

HS1 family of prop airfoils

HS1708 Airfoil (x,y) Co-ordinates

0 0.00013
0.0005 0.0033
0.001 0.00479
0.002 0.00704
0.003 0.00883
0.005 0.01173
0.0075 0.01461
0.01 0.01704
0.02 0.02448
0.03 0.03017
0.04 0.03501
0.05 0.03932
0.06 0.04326
0.07 0.04692
0.08 0.05031
0.09 0.05344
0.1 0.05634
0.12 0.06151
0.14 0.06595
0.16 0.06977
0.18 0.07308
0.2 0.07587
0.22 0.07824
0.24 0.08021
0.26 0.08182
0.28 0.08313
0.3 0.08421
0.34 0.08583
0.36 0.0864
0.38 0.0868
0.4 0.08701
0.44 0.08681
0.46 0.0864
0.48 0.08579
0.5 0.08502
0.54 0.08301
0.56 0.08176
0.58 0.08033
0.6 0.07865
0.64 0.07443
0.66 0.07184
0.68 0.06892
0.7 0.0657
0.74 0.05853
0.76 0.05465
0.78 0.05062
0.8 0.04649
0.82 0.04221
0.84 0.03798
0.86 0.0336
0.88 0.02916
0.9 0.02462
0.91 0.02231
0.92 0.01996
0.93 0.01757
0.94 0.01512
0.95 0.01262
0.96 0.01005
0.97 0.00741
0.98 0.00471
0.99 0.00196
1 -0.00086
1 -0.00734
0.99 -0.00652
0.98 -0.00572
0.97 -0.00493
0.96 -0.00416
0.95 -0.00341
0.94 -0.00268
0.93 -0.00196
0.92 -0.00128
0.91 -0.00058
0.9 0.00006
0.88 0.00133
0.86 0.00248
0.84 0.00356
0.82 0.00459
0.8 0.00557
0.78 0.0065
0.76 0.00738
0.74 0.00818
0.7 0.00947
0.68 0.00996
0.66 0.01034
0.64 0.01065
0.6 0.01105
0.58 0.01118
0.56 0.01125
0.54 0.01129
0.5 0.0112
0.48 0.01106
0.46 0.01087
0.44 0.0106
0.4 0.00984
0.38 0.00932
0.36 0.00868
0.34 0.00791
0.3 0.00583
0.28 0.0045
0.26 0.00293
0.24 0.00113
0.22 -0.00092
0.2 -0.00318
0.18 -0.00559
0.16 -0.00808
0.14 -0.0105
0.12 -0.01271
0.1 -0.01456
0.09 -0.0153
0.08 -0.01588
0.07 -0.01629
0.06 -0.0165
0.05 -0.01645
0.04 -0.01603
0.03 -0.01506
0.02 -0.01322
0.01 -0.0099
0.0075 -0.00865
0.005 -0.00715
0.003 -0.00561
0.002 -0.00485
0.001 -0.00338
0.0005 -0.00244
0 0.00013

HS1708 Airfoil CAD files

DOWNLOAD FROM HERE

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